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SAE International

SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
2011-01-2585
Integrated Engine/Thermal Architecture Model Interface Development
 
2011-01-2625
Silicon Carbide Power Electronics for High-Temperature Power Conversion and Solid-State Circuit Protection in Aircraft Applications
 
2011-01-2584
Two Phase Thermal Energy Management System
 
2011-01-2586
Vapor Cycle Compressor Range Expansion for Aerospace
 
2010-01-1725
A Framework for Developing an EPS Health Management System
V119-1  
2010-01-1791
A Fuel-Cell Electric Vehicle with Cracking and Electrolysis of Ammonia
 
2010-01-1786
A Hybrid Economy Bleed, Electric Drive Adaptive Power and Thermal Management System for More Electric Aircraft
V119-1  
2010-01-1778
A Method of Shared Regenerative Power Management
 
2010-01-1813
A Methodology to Predict Axial Clamping Force and Anti-rotating Torque for V-band Joint
 
2010-01-1756
A Modular Power System Architecture for Military and Commercial Electric Vehicles
 
2010-01-1741
A Reduced-Order Enclosure Radiation Modeling Technique for Aircraft Actuators
 
2010-01-1752
A Scalable Hybrid Power and Energy Architecture for Unmanned Ground Vehicles
 
2010-01-1753
Actuator Remaining Life Estimation Under Fault Tolerant Operation
 
2010-01-1750
Adaptive Protection Methods for Aircraft Applications
 
2010-01-1758
Advanced Electric Generators for Aerospace More Electric Architectures
 
2010-01-1799
Air-Launched Expendable Small Unmanned Aircraft Systems: Increasing Power and Extending Endurance to Meet Operational Needs
 
2010-01-1807
An Algebraic-Summation-Based 3-ph Phase-Locked Loop in Aerospace Applications
 
2010-01-1744
An Electromechanically Actuated Nose Landing Gear Using a Dual-Output Motor Control Unit
 
2010-01-1746
An Overview of Electrically Powered Control Actuation Health Management
 
2010-01-1740
Analysis and Reduction of Common-Mode EMI in Electric Actuators for VF MEA
 
2010-01-1729
Assessment of High-Temperature Encapsulants for Planar Packages
 
2010-01-1806
Automated Model Evaluation and Verification of Aircraft Components
 
2010-01-1737
Constrained Dynamic Inversion Control and Its Application to Turbomachinery
 
2010-01-1747
Control Strategy for Electro-Mechanical Actuators Versus Hydraulic Actuation Systems for Aerospace Applications
 
2010-01-1764
Controlling and Monitoring Linear Actuators via the Power Distribution System
 
2010-01-1757
Converging Technologies for Electric/Hybrid Vehicles and More Electric Aircraft Systems
 
2010-01-1789
DME Hybrid Power System with CO2 Recycling for Commercial Vehicles
 
2010-01-1726
Development of Self-Healing High Temperature Film Capacitors for Power Electronics Applications
 
2010-01-1800
Double Bypass Turbofan Engine Modeling including Transient Effects
 
2010-01-1748
Dynamic Testing of Electromechanical Actuators Using Time-history Data
 
2010-01-1809
Effects of Line and Load Conditions on TRU and ATRU Input Current Harmonics
 
2010-01-1736
Electronics Cooling Using High Temperature Loop Heat Pipes With Multiple Condensers
 
2010-01-1768
Enhanced Identification Algorithms for Battery Models under Noisy Measurements
 
2010-01-1734
Enhanced Specific Heat Capacity of Molten Salt-Metal Oxide Nanofluid as Heat Transfer Fluid for Solar Thermal Applications
 
2010-01-1793
Evaluating High Temperature/High Voltage Packaging for SiC Power Electronics
 
2010-01-1733
Evaluation of a Vapor-Compression Thermal Management System for Reliability While Operating Under Thermal Transients
 
2010-01-1731
Experimental Validation of a Simple Analytical Model for Specific Heat Capacity of Aqueous Nanofluids
 
2010-01-1787
Facilitating the Energy Optimization of Aircraft Propulsion and Thermal Management Systems through Integrated Modeling and Simulation
 
2010-01-1766
Fault Mitigation and Cell Balancing of High Power Lithium Ion Battery Packs
 
2010-01-1743
Fault-Tolerant Electrical Motor Drives for Aerospace Application
 
2010-01-1795
HV Design Guidelines on Aerospace (and Air) Vehicles
 
2010-01-1810
Hardware-in-the-Loop Electric Drive Stand Issues for Jet Engine Simulation
 
2010-01-1727
High Temperature Capable Ionic Polymer-Metal Composite Capacitors and Power Storage Systems
 
2010-01-1798
High Temperature, High Frequency SiC Three Phase Inverter for Aircraft Applications
 
2010-01-1780
Improving Peak Power Capability of an Aircraft
 
2010-01-1804
Integrated Aircraft Electrical Power System Modeling and Simulation Analysis
 
2010-01-1812
Integrated Electrical and Thermal Management Sub-system Optimization
 
2010-01-1742
Integrated Nonlinear Dynamic Modeling and Field Oriented Control of Permanent Magnet (PM) Motor for High Performance EMA
 
2010-01-1776
Integration of a Microtubular Solid Oxide Fuel Cell into a Mini-UAV: Design and Simulation of Power System Architecture
 
2010-01-1754
Inverter-Motor System EMI Reduction by Impedance Balancing
 
2010-01-1735
Investigation of Thermal Characteristics of Nanofluids During Flow in a Micro-channel Using an Array of Surface Temperature-Nano-Sensors
 
2010-01-1785
Investigation of Tradeoffs between Efficiency, Mass, Cost, Service Factor, and Power Factor in Induction Machines
V119-1  
2010-01-1749
Lumped Node Thermal Modeling of EMA with FEA Validation
 
2010-01-1761
Model Based Diagnostics of an Aircraft Generator Using AAKR and SPRT
V119-1  
2010-01-1777
Modular Digital Power Factor Correction for Aerospace Applications
 
2010-01-1745
More Electrical Actuation for ATA 32 : Modular Power Electronics & Electrical Motor Concepts
 
2010-01-1788
Potential Technology to Unclog Hot Day Operational Limit
 
2010-01-1738
Power Flow Analysis for a Two-stage Direct Power Converter for Use in an Aircraft Aileron Application
 
2010-01-1805
Power Thermal Management System Design for Enhanced Performance in an Aircraft Vehicle
 
2010-01-1751
Practical Hybrid Contactors
 
2010-01-1792
Practical Requirements for New High-Temperature Batteries In Drilling
 
2010-01-1790
Radial Accelerated Cavitation and its use in Fuel Reformation
 
2010-01-1782
Reconfigurable Aircraft DC Power Networks Laboratory
 
2010-01-1801
Region of Asymptotic Stability Estimation with Lyapunov Function Optimization and the Average Derivative Method
 
2010-01-1765
SOH Recognition of Li-ion Aviation Batteries Via Passive Diagnostic Device
 
2010-01-1762
SoH Recognition of Aviation Batteries Via Passive Diagnostic Device
V119-1  
2010-01-1755
Standardized Electrical Power Quality Analysis in Accordance with MIL-STD-704
V119-1  
2010-01-1770
System Integration of a Safe, High Power, Lithium Ion Main Battery into a Civil Aviation Aircraft
V119-1  
2010-01-1779
The Modular Design of an Aircraft Power Distribution System
 
2010-01-1732
Thermal Analysis of Carbon Nanotubes Suspended in PAO Mixtures
 
2010-01-1781
Thermal Management and Power Generation for Directed Energy Weapons
 
2010-01-1728
Thermo-Mechanical Reliability of Nano-Silver Sintered Joints versus Lead-Free Solder Joints for Attaching Large-Area Silicon Devices
 
2010-01-1767
Tracking Over Insulating Surfaces In Aerospace Environments
 
2010-01-1784
Vacua Buoyancy Is Provided by a Vacuum Bag Comprising a Vacuum Membrane Film Wrapped Around a Three-Dimensional (3D) Frame to Displace Air, on Which 3D Graphene “Floats” a First Stack of Two-Dimensional Planer Sheets of Six-Member Carbon Atoms Within the Same 3D Space as a Second Stack of Graphene Oriented at a 90-Degree Angle
 
2009-01-3219
A Direct Torque-Controlled Induction Machine Bidirectional Power Architecture for More Electric Aircraft
V119-1  
2009-01-3162
Advanced Electrical Signature Analysis of Aircraft Electrical Generators
V119-1  
2009-01-3192
An Acoustic-Based Wiring Diagnostic System for Aircraft
 
2009-01-3161
Applying Poincaré Plots for Evaluating the Health State of Aircraft Generators
V119-1  
2009-01-3188
Comparative Test Results of a Brushless DC Starter Generator vs. Traditional Starter Generator with Brushes
 
2009-01-3163
Condition Based Maintenance for Aircraft Electrical Systems
 
2009-01-3191
Electrochemical Testing at SAFT to Support Health Prognostication Management for Aviation
 
2009-01-3122
Electronic Power Distribution System Topologies
 
2009-01-3164
Equipment Condition Monitoring and Prognostic Methods for Single Variable Systems
 
2009-01-3133
Flying Test Bed Performance Testing of High-Bypass-Ratio Turbofans
V118-1  
2009-01-3159
High Altitude Platforms for Telecommunications: Design Methodology
 
2009-01-3124
High Temperature Multilayer Ceramic Capacitors
V119-1  
2009-01-3189
Improving Load Regeneration Capability of an Aircraft
 
2009-01-3190
Integrating Electrical Prognostics and Monitoring into an Electronic Power Distribution System
 
2009-01-3238
Lightweight, Portable Power Solutions for Soldiers on Dismounted Missions, Mobile Reliable Power for Manned and Unmanned Vehicles
 
2009-01-3134
Method and System for Making a Fuel-tank Inert without an Inert Gas
V118-1  
2009-01-3120
Power Line Communication Techniques for Multi-User and Higher Data Rate Applications in an Aircraft
 
2009-01-3220
Power and Energy Balance for Model Validation and Reduction (PEMRA) – Frequency Coupling. Application on Aircraft System Models
 
2009-01-3217
Recent Advances Towards an Integrated and Optimized Design of High Lift Actuation Systems
V119-1  
2009-01-3121
Role of Power Distribution System Tests in Final Assembly of a Military Derivative Airplane
V119-1  
2009-01-3095
Stator Side Voltage Regulation of Permanent Magnet Generators
V119-1  
2009-01-3093
Thermoelectric Energy Harvesting from Small Aircraft Engines
 
2009-01-3103
Variable Pitch Fan - The Solution to Achieving High Propulsive Efficiency Turbofan Engines
 
2008-01-2892
250 °C SiC Power Module Package Design
 
2008-01-2877
400Hz High Speed Static Transfer Switch
V117-1  
2008-01-2883
4H-SiC VJFET Based Normally-off Cascode Switches for 300°C Electronic Applications
V117-1  
2008-01-2907
A Battery Electronics Unit (BEU) for Balancing Lithium-Ion Batteries
 
2008-01-2875
A Comparison of Lithium-Ion and Lead-Acid Aircraft Batteries
 
2008-01-2887
A Dynamic Surrogate Model Technique for Power Systems Modeling and Simulation
 
2008-01-2914
A General Aviation Aircraft Retrofit with a PEM Fuel Cell
 
2008-01-2872
A Novel Position Sensorless Control Approach for Synchronous Electrical Machines for Aerospace Applications
 
2008-01-2925
A Review of Alternative Electrical Power Distribution Methods for Future Unmanned Aerial Vehicles
 
2008-01-2870
A Survey on Arc Fault Detection and Wire Fault Location for Aircraft Wiring Systems
V117-1  
2008-01-2923
Advanced Diagnostics of Aircraft Electrical Generators
V117-1  
2008-01-2861
Advanced Electric Drives for Aerospace More Electric Architectures
V117-1  
2008-01-2895
Advanced FeF3 Cathode Enabled Lithium-ion Battery
V117-1  
2008-01-2903
Advanced Heat Exchanger Technology for Aerospace Applications
 
2008-01-2893
Advanced High Energy and High Power Battery Designs and Materials for UAVs, UUVs and UMVs
 
2008-01-2922
Advanced Prognostics for Aircraft Electrical Power Systems
V117-1  
2008-01-2918
Aerospace Power Electronics Radiation Heat Transfer Considerations
 
2008-01-2890
Aircraft DC Power Quality Characteristics of a PCTRU
V117-1  
2008-01-2917
Approach for an Integrated Multi-Domain Aircraft Energy Model
V117-1  
2008-01-2905
Comparative Analysis of Thermal Management Architectures to Address Evolving Thermal Requirements of Aircraft Systems
 
2008-01-2854
Comparison of Four Fuel Cell Battery Hybrid Powertrains in Bus Applications
 
2008-01-2888
Considerations for V-22 Electrical Power System Improvements
 
2008-01-2871
Design Considerations for Aircraft Generator with Start Function
 
2008-01-2865
Design Considerations when Disproportionate Heating of Lithium-ion Battery Packs is Present
V117-1  
2008-01-2930
Design of Compact, Lightweight Power Transmission Devices for Specialized High Power Applications
V117-1  
2008-01-2867
Designing for Large-Displacement Stability in Aircraft Power Systems
V117-1  
2008-01-2884
Development and Test of Safe, High Power Lithium Ion Main Batteries for General Aviation Aircraft
V117-1  
2008-01-2851
Development of High Temperature Capacitors for High Density, High Temperature Applications
V117-1  
2008-01-2891
Digital Control of High Temperature SiC Power Modules Utilizing HTSOI
V117-1  
2008-01-2911
Dynamic Circuit Analysis and Testing for International Space Station Science Experiments
 
2008-01-2886
Dynamic Thermal Management System Modeling of a More Electric Aircraft
 
2008-01-2908
Early Validation of Power Distribution Channel Controller LRM Requirements using Rapid Prototyping Simulation
 
2008-01-2926
Effects of Transient Power Extraction on an Integrated Hardware-in-the-Loop Aircraft/Propulsion/Power System
 
2008-01-2927
Electrical Accumulator Unit for the Energy Optimized Aircraft
V117-1  
2008-01-2919
Enabling Much Higher Power Densities in Aerospace Power Electronics with High Temperature Evaporative Spray Cooling
 
2008-01-2900
Evaluation of Overvoltage Protection Requirements for a DC UAV Electrical Network
 
2008-01-2860
Examination of Aircraft Electric Wheel Drive Taxiing Concept
 
2008-01-2896
Expanding the Temperature Range of High Power Lithium-Ion Chemistry
V117-1  
2008-01-2859
Fast Reduced Functional Models of Electromechanical Actuators for More-Electric Aircraft Power System Study
 
2008-01-2909
Hardware-in-the-Loop Power Extraction Using Different Real-Time Platforms
 
2008-01-2928
Heat Transfer Performance of a Dual Latent Heat Sink for Pulsed Heat Loads
V117-1  
2008-01-2885
High Performance Lithium Ion Aircraft Battery for DoD Platforms
 
2008-01-2866
High Power Lithium Ion Battery Facilitated by an Advanced Cathode
 
2008-01-2863
High Temperature Sodium Bismuth Titanate Capacitors – A New Product Realized
V117-1  
2008-01-2850
High Voltage Metal Oxide Varistors for Surge Protection
 
2008-01-2853
High-Temperature, High-Power Capacitors: the Assessment of Capabilities
V117-1  
2008-01-2920
Hybrid Thermosyphon for Power Electronics Thermal Management in High Gravity Applications
 
2008-01-2876
Inductive Load Switching Suppression Methods: Increasing Military and Aerospace Applications Reliability
V117-1  
2008-01-2924
Integrated Diagnostics of AC Machines with Time-Shared Embedded Digital Control System for Aircraft Applications
 
2008-01-2899
Integrated Electrical System Model of a More Electric Aircraft Architecture
 
2008-01-2897
Integrated Electrical System Testing and Modeling for Risk Mitigation
 
2008-01-2879
Interfacing Power Line Communications to Airborne Vehicles: A Technical Review
 
2008-01-2932
Intermittent Fault Location on Live Electrical Wiring Systems
V117-1  
2008-01-2901
Lunar RFC Reliability Testing for Assured Mission Success
V117-1  
2008-01-2906
Minimum Operation Performance Standard for Aircraft Batteries
 
2008-01-2868
Modeling and Analysis of Bus Voltage Control in Aerospace Applications
 
2008-01-2857
Modeling and Analysis of a Phasor-Controlled ME/APU S/G in Motoring Mode
 
2008-01-2858
Modeling, Analysis, and Control Design for an Intermittent Megawatt Generator
V117-1  
2008-01-2855
Multi-Fuel Reforming and Fuel Cell Systems for Aviation Applications: The Role of Bio-Diesel and its Synergy with Global Interests
 
2008-01-2921
Next Generation Li-Ion Technology from SAFT
 
2008-01-2934
Next Generation Power and Thermal Management System
V117-1  
2008-01-2878
Overview of Multiphase Power Converters for Aerospace Applications
 
2008-01-2931
Physics and Measurement of Early Wire Insulation Chafing
V117-1  
2008-01-2852
Polyimide Flex Circuitry for >200C
 
2008-01-2894
Prismatic Li-Ion Cell for Unmanned Aircraft
V117-1  
2008-01-2916
Reconfiguration of Distribution System Feeder Using Slope Criterion
 
2008-01-2898
Regeneration in Aircraft Electrical Power Systems?
 
2008-01-2873
Roles of Active Rectifiers in the Future Aircraft Power Systems
 
2008-01-2874
Small Turbine Engine Evolution
V117-1  
2008-01-2869
Small-Signal Input Impedance Modeling of Multipulse Rectifiers
 
2008-01-2902
Speed Control Method for Turboelectric Power Generation Systems
 
2008-01-2933
State of Health Recognition for Aircraft Batteries Dynamic Equivalent Schematic and First Principles Model Considerations
 
2008-01-2862
Superconducting Machines and Power Systems for Electric-Drive Aeropropulsion
V117-1  
2008-01-2929
System Performance and Characteristics of High-Speed HTS Generators
 
2008-01-2910
TRU and ATRU Analysis by Matrix Methods
V117-1  
2008-01-2889
TRU with Low Input Voltage Boost for 28VDC Aircraft Power Systems
 
2008-01-2882
Test of SOI 555 Timer with High Temperature Packaging
V117-1  
2008-01-2856
The Direct Methanol Fuel Cell (DMFC): Determination of Model Parameters
V117-1  
2008-01-2904
Thermal-Hydraulic Performance of Microstructured Heat Exchangers
V117-1  
2008-01-2913
Using Datasheet Information to Predict the Power Dissipation of a Hybrid Silicon Carbide IGBT Module in a Voltage Source Inverter
 
2008-01-2864
Wind Energy Harvesting for Low Power Applications
V117-1  
2008-01-2880
“Smart Panel” Electronic Circuit Breaker Control Technology
 
2007-01-3789
A Mean Value Based Sizing and Simulation Model of a Hydrogen Fueled Spark-Ignition Internal Combustion Engine
 
2007-01-3790
A Step Towards CO2-Neutral Aviation
 
2007-01-3861
Application of Non-Parametric Statistical Methods to Reliability Database Analysis
 
2007-01-3864
Case for a Multidisciplinary Modeling Platform for Space Launch Risk Analysis
 
2007-01-3932
Evaluation of a Mixed Flow Turbofan Engine with Intermediate Turbine Burning for a Supersonic Aircraft
 
2007-01-3876
Liquid Oxygen/Liquid Methane Rocket Engine Development
 
2007-01-3860
Soviet Propeller V/STOL Concepts of the 20th Century
 
2007-01-3859
Status, Vision, and Challenges of an Intelligent Distributed Engine Control Architecture
 
2006-01-3099
3.2 KWH Battery Pack Using 18 Army Standard Lithium ion Rechargeable Batteries
 
2006-01-3074
A 10KW Modular Inverter for 28 VDC to 120/240 VAC Power Conversion
 
2006-01-3070
A Novel Control Scheme to Increase Electrical Torque of a Drive System for Aircraft Main Engine and APU Start
 
2006-01-3031
AC-link™ Converter Topology for Power-Dense AC and DC Applications
 
2006-01-3023
Advanced Bipolar Lithium Ion Battery
 
2006-01-3088
Advances in Active Power Converter Topologies for Power Quality Solution for More Electric Aircraft
 
2006-01-3093
Aeronautical Fuel Cell System Application and Associated Standardization Work
 
2006-01-3081
Aircraft Battery Design Concept for Improved Ultra Low Temperature Performance
 
2006-01-3079
Aircraft Battery Servicing Systems
 
2006-01-3091
Aircraft Electrical System Monitoring with Arc Fault Circuit Protection and Automatic Fault Location
 
2006-01-3028
Aircraft High-Power Semiconductor Line Contactors
 
2006-01-3066
Aircraft Thermal Management Using Loop Heat Pipes: Experimental Simulation of High Acceleration Environments Using the Centrifuge Table Test Bed
 
2006-01-3056
Altitude Performance Test Results for Low Pressure Turbine Mounted Generator
 
2006-01-3036
An Automated Average-Value Modeling Methodology for Power Electronic Sources and Loads
 
2006-01-3061
An Electric Power Generation System for Launch Vehicles
 
2006-01-3105
Applications for High-Temperature (HT) Power Electronic Systems within the Drilling Industry
 
2006-01-3090
Arc Fault Detection through Model Reference Estimation
 
2006-01-3045
Automated Evolutionary Design of a Hybrid-Electric Vehicle Power System Using Distributed Heterogeneous Optimization
 
2006-01-3022
Cell Equalization of Lithium Ion Cells
 
2006-01-3065
Centrifuge Testing of a Partially-Confined FC-72 Spray
 
2006-01-3051
Closed Loop Controlled High Speed Induction Generators Using Adaptive Control Technique
 
2006-01-3048
Coupled-Circuit Modeling of 3, 6, and 9-Phase Induction Machine Drive Systems
 
2006-01-3042
Distributed Heterogeneous Simulation of a Hybrid-Electric Vehicle Drive System Using the Simplorer Software Product
 
2006-01-3080
E-6 and E-3 Main Battery and Charger Upgrade
 
2006-01-3068
Effect of Thermal Conductivity and Latent Heat of Vaporization of Liquid on Heat Transfer in Spray Cooling
 
2006-01-3064
Electrical Force Effects on Spray Cooling
 
2006-01-3039
Electrical Modeling and Simulation with Matlab/Simulink and Graphical User Interface Software
 
2006-01-3053
Electrical System Evaluation Platform for Uninhabited Autonomous Vehicles
 
2006-01-3024
Evaluation of Life Cycle Performance of Lithium Ion Cells for Space Applications
 
2006-01-3101
Field Auxiliary Power Unit using Advanced Large Format Lithium-Ion Cells
 
2006-01-3054
GCU for Megawatt Class Directed Energy Weapons Pulse Generators
 
2006-01-3027
High Efficiency Cockpit Instrument Lamp Dimmers, An Overview
 
2006-01-3033
High Power Semiconductor Switching
 
2006-01-3098
High Specific Energy Rechargeable Battery for the Tactical Warfighter
 
2006-01-3025
High Temperature Battery for Space Applications
 
2006-01-3106
High Temperature Packaging and Pulse Testing of Parallel SiC Thyristors
 
2006-01-3096
High Temperature Polymer Electrolyte Membrane Fuel Cells (HT-PEMFCs) for Portable Power
 
2006-01-3076
High-Reactance Permanent Magnet Machine for High-Performance Power Generation Systems
 
2006-01-3089
Hybrid Power Generation for Achieving Airship Neutral Buoyancy
 
2006-01-3044
Improvements in the Distributed Heterogeneous Simulation of Aircraft Electric Power Systems
 
2006-01-3035
Integrated Hardware-in-the-Loop Simulation of a Complex Turbine Engine and Power System
 
2006-01-3043
Modeling Approach for the Integrated Secondary Electric Power Distribution System with Solid State Power Controllers
 
2006-01-3038
Modeling Considerations and Stability Analysis of Aerospace Power Systems with Hybrid AC/DC Distribution
 
2006-01-3046
Modeling and Analysis of a Main Engine Start Power Flow
 
2006-01-3050
Modeling and Simulation of an Electric Warship Integrated Engineering Plant
 
2006-01-3059
Multi-Objective Optimization of Spacecraft Electrical Power Subsystem Design/Sizing
 
2006-01-3082
NiCd Battery Performance for Aircraft Applications
 
2006-01-3041
Nonlinear Electrical Simulation of High-Power Synchronous Generator System
 
2006-01-3063
Pool Boiling Experiments Using Surface Micromachined Thermocouples
 
2006-01-3086
Power Conversion Technologies for Reducing Harmonics on the More Electric Aircraft
 
2006-01-3058
Power Distribution for Spacecraft Payloads that Employ State of the Art Radiation Hardened Integrated Circuits
 
2006-01-3034
Power Management Software Interfaces Standard
 
2006-01-3102
Real-time Thermal Observer for Electric Machines
 
2006-01-3083
Rechargeable Lithium-Ion Based Batteries and Thermal Management for Airborne High Energy Electric Lasers
 
2006-01-3095
Reformation of Jet Fuels for Navy Ground Cart Applications
 
2006-01-3084
Replacement of Sealed Nickel-Cadmium Batteries on EA-6B Aircraft with Valve Regulated Lead-Acid Batteries
 
2006-01-3077
Robust Control Techniques Enabling Duty Cycle Experiments Utilizing a 6-DOF Crewstation Motion Base, a Full Scale Combat Hybrid Electric Power System, and Long Distance Internet Communications
 
2006-01-3021
SAFT Li-ion Technology for High Rate Applications
 
2006-01-3071
Study on Main Engine Start for More Electric Architecture Aircraft
 
2006-01-3026
Super NiCd Applications and Mission History
 
2006-01-3078
Switching Harmonics in a Three-Phase PWM Inverter
 
2006-01-3062
System Evaluation of Cavitation Enhanced Heat Transfer in Microchannels
 
2006-01-3092
Test Results for a Fuel Cell-Powered Demonstration Aircraft
 
2006-01-3100
The Bipolar Nickel Metal Hydride High Energy Army Silent Watch Battery
 
2006-01-3020
The Bipolar Nickel-Metal Hydride Battery for Advanced Transportation and High Voltage Power and Energy Storage Systems
 
2006-01-3067
The Heat Transfer Effects of Nanotube Surfaces Treatments and a Means for Growing the Nanotube Coated Surfaces
 
2006-01-3055
The Quest for Oil-Free Gas Turbine Engines
 
2006-01-3107
Total Battery Management System for Aviation Batteries
 
2006-01-3097
Towards Electric Aircraft: Progress under the NASA URETI for Aeropropulsion and Power Technology
 
2006-01-3040
Transient Turbine Engine Modeling and Real-Time System Integration Prototyping
 
2006-01-3108
Turbomachinery Aero Design; Getting It Right the First Time
 
2005-01-3413
A New Approach for Single Stage Ascent to Orbit Silane Fuel in a New Vehicle Design
 
2005-01-3192
A Propulsion Concept for Circulation Control Wing Technology
 
2005-01-3374
A Propulsion Device for Spacecraft
 
2005-01-3347
Airline Regulation to Deregulation; It’s Not Over Yet!
 
2005-01-3424
Crash Analysis of a Command and Control System Deployed on the Rear Ramp of a C-130 Aircraft
 
2005-01-3197
Design Guidelines for Flapping-Wing Micro UAVs
 
2005-01-3388
Design of D-B Injectors for Increasing Propulsive Force in Jets
 
2005-01-3166
Development of a Radio-Controlled Ornicopter: a Single Rotor Helicopter Without Reaction Torque
 
2005-01-3186
Ducted Fan Efficiency and Noise
 
2005-01-3182
Empirical Wake Turbulence Model of Tiltrotor Aircraft
 
2005-01-3193
Engineering Solutions for Circulation Control Applications
 
2005-01-3177
Executive Summary of Cal Poly/NASA Extreme Short Takeoff and Landing (ESTOL) Work
 
2005-01-3426
Experimental Stress/Strain Analysis of a Standardized Sensor Platform for a C-130 Aircraft
 
2005-01-3171
Experimental and Computational Studies of Unsteady Flow Features of Upwash Fountains from Twin Impinging Jets
 
2005-01-3200
Exploratory Business Case Study for an Extreme Short Take-Off and Landing Transport
 
2005-01-3425
Hub Connection Simulation of a Sensor Platform System
 
2005-01-3168
Inclusion of the Rotor Speed Degree of Freedom for Substantial Increases In Advanced Rotorcraft Performance and Safety
 
2005-01-3427
Maintenance Issues and Fail Safes of the Oculus Sensor Platform System
 
2005-01-3180
Motion-Based Flight Simulator Usage for F-35 Control Law Development
 
2005-01-3149
NASA Heavy Lift Rotorcraft Systems Investigation
 
2005-01-3389
Reliability of the Engine Electronic Controls and a Novel Approach to Improve Service Life
 
2005-01-3412
Silicon Based Fuels for Space Flight
 
2005-01-3169
Simultaneous Non Interfering (SNI) Operations, FAA Research, Development, and Implementation Efforts
 
2005-01-3199
Some Non-linear Aerodynamics Relevant to Flapping-wing MAVs
 
2005-01-3158
State of the Art in Sub-scale STOVL Hot Gas Ingestion Wind Tunnel Test Techniques
 
2005-01-3145
Summary of NASA's Extreme Short Take-Off and Landing (ESTOL) Vehicle Sector Activities
 
2005-01-3390
System Software Safety Assessment Process for Certification of Commercial and Military Aircraft
 
2005-01-3173
The Development and Implementation of a New Surface Erosion Measurement Technique
 
2005-01-3153
Unsteady Fuselage Loads on Rotorcraft in Ground Effect
 
2005-01-3183
Volantor - A Powered Lift Aircraft for Personal Use
 
2005-01-3198
Wake Structure Diagnostics of a Flapping Wing MAV
 
2004-01-3126
Built-In Test in Fiber Optic Links - Enabling Technology for a Network-Centric Future
 
2004-01-3085
Design and Evaluation of Novel Composite Aircraft Repairs
 
2004-01-3124
Design of a Roadable Aircraft of Fixed Wing and the Investigation of the Aerodynamic Characteristics
 
2004-01-3138
Flight Characterization of Micro Air Vehicles Using Morphing for Agility and Maneuvering
 
2004-01-3111
Influence of Strain Rates on Springback of 2xxx Series Aluminum Alloys
 
2004-01-3137
Maneuvering and Tracking for a Micro Air Vehicle Using Vision-Based Feedback
 
2004-01-3127
Methodology for the Conceptual Design Process of Morphing Configurations
 
2004-01-3125
RF Photonics For Aerospace Applications
 
2004-01-3086
Reliability of Electronic Engine Controls
 
2004-01-3100
Simulation Study of a Commercial Transport Airplane During Stall and Post-Stall Flight
 
2004-01-3112
The Effect of Forming Pressure on Springback in 2XXX Aluminum Alloys
 
2004-01-3128
The More Electric Engine Concept
 
2004-01-3108
Water Injection: Disruptive Technology1 to Reduce Airplane Emissions and Maintenance Costs
 
2003-01-3051
A Technique for Use of Gaussian Processes in Advanced Meta-Modeling
 
2003-01-3058
Aerospace Systems Design: Economics as a New Way of Thinking?
 
2003-01-3064
American Attack Unmanned Aerial Vehicles (UAVs): A Century of Progress
 
2003-01-3050
Beyond the Harrier - Kingston V/Stol Projects 1957-1988
 
2003-01-3068
Class D to Class C Cargo Compartment Conversions for Fire Protection Systems in Transport Category Aircraft
 
2003-01-3016
Design and Evaluation of Novel Composite Aircraft Repairs
 
2003-01-3020
Downwash Wake Reduction Investigation for Application on the V-22 “Osprey”
 
2003-01-3029
Fluoroelastomer and Perfluoroelastomer Compatibility With Advanced Gas Turbine Lubricants
 
2003-01-3015
Globalization of Commercial Aircraft Manufacturing
 
2003-01-3055
Implementation of a Physics-Based Decision-Making Framework for Evaluation of the Multidisciplinary Aircraft Uncertainty
 
2003-01-3063
Productivity Metrics for Business and Regional Aircraft
 
2003-01-3059
Response Surface Utilization in the Exploration of a Supersonic Business Jet Concept with Application of Emerging Technologies
 
2003-01-3038
SATS Life Cycle Costs in an Air Taxi Operation
 
2003-01-3017
“A Dry Aircraft is a Safer Aircraft – Beating Condensation by Using Dry Air”
 
2003-01-2671
Evaluation of Sample Preservation Methods for Space Missions
 
2002-01-2949
A Longitudinal Slip Tire Model for Brake Control Systems: Features and Uses in Simulation, Control Synthesis and Stability Analysis
 
2002-01-2958
ATN Airborne Implementation
 
2002-01-2963
Airline Pilots' Perceptions of and Experiences in Crew Resource Management (CRM) Training
 
2002-01-2965
An Automated System Framework for Pre-Mission Success Evaluation of Medical Emergency Helicopters Operations – Derived Mission Capability Sub-Module
 
2002-01-2916
Assessment of the Dynamic Stability Characteristics of the Bell Model M427 Helicopter Using Parameter Estimation Technology
 
2002-01-2948
Asymmetric Approach in Solving Aircraft Brake Vibration
 
2002-01-2968
Designing User-Interfaces for the Cockpit: Five Common Design Errors and How to Avoid Them
 
2002-01-3012
Determining Optimum Redesign Plans for Avionics Based on Electronic Part Obsolescence Forecasts
 
2002-01-2925
Development and Application of a Real Time Bleed Air Contamination Monitor
 
2002-01-2947
Development of Reduced Catalytically Active Runway Deicer Fluids for Carbon/Carbon Composite Friction Materials
 
2002-01-2924
Economic Viability of NASA's Next-Generation Aviation Paradigm: A Summary of Research Findings
 
2002-01-2953
Electric Starting of Large Aircraft Engines
 
2002-01-2945
End Item Temperature Test -- An Improved LRU-Level Screen
 
2002-01-2998
Enhanced Security Flight Deck Doors-Commercial Airplanes
 
2002-01-2941
Environmental Systems Considerations for Aircraft Cabins During Ground Operation
 
2002-01-3001
FEA Cyclic Symmetric Fatigue Analysis of Aircraft Wheels
 
2002-01-2957
Fire Resistant Composites
 
2002-01-2931
Fuel Transfer System in the Conceptual Design Phase
 
2002-01-3006
HUD Symbology for Surface Operations: Command Guidance vs. Situation Guidance Formats
 
2002-01-3008
Highlights of NASA's Systems Approach to Crashworthiness Research
 
2002-01-2956
Hybrid-Ceramic Circumferential Carbon Ring Seal
 
2002-01-2927
Identification and Evaluation of Technologies for the Development of a Quiet Supersonic Business Jet
 
2002-01-2930
Impact of Configuration and Requirements on the Sonic Boom of a Quiet Supersonic Jet
 
2002-01-2990
Improving the Aerodynamic Efficiency of High Lift Devices by a Stiffness Oriented Re-design with Tailored Laminates
 
2002-01-3010
Incorporation of Lean Principles through the use of Flexible Fuel Tubing in a Large Military Transport Aircraft
 
2002-01-3004
Metastable Beta Titanium Spring Performance at Elevated Temperature
 
2002-01-2942
Method for Analyzing Lubricating Oil Contamination of Aircraft Systems
 
2002-01-2918
Model of Casing Treatment Influence on Compressor Rotor Efficiency
 
2002-01-2974
One-Pass Pricing Methodology
 
2002-01-2944
Past, Present, and Future of the Gas Turbine Engine Simulator; A Technical and Financial Analysis
 
2002-01-3000
Photon Induced Positron Annihilation (PIPA)—A New, Core Technology to Improve the Nondestructive Inspection and Life Prediction for Critical Components
 
2002-01-3011
Plastic Ball-Grid-Arrays (PBGA): Are they ready for environmentally harsh Aerospace applications?
 
2002-01-2926
Propulsion Education for General Aviation Aircraft
 
2002-01-2929
Quiet Supersonic Jet Engine Performance Tradeoff Analysis Using a Response Surface Methodology Approach
 
2002-01-2967
Rear Projection for Multi-Function Displays
 
2002-01-2983
Recommendations for Future Avionics Hardware Development
 
2002-01-2922
Relative Guidance of Aircraft: Analysis and Comparison of Two Control Approaches
 
2002-01-2951
Reliable Bearing Wear Detection System for On-Condition Maintenance of Electric Generators
 
2002-01-2954
Sensorless Control of Brushless DC Motor for More Electric Aircraft
 
2002-01-2985
Software Tools for the Development of Design Decision Support for Re-Configurable Unmanned Arial Vehicles
 
2002-01-2928
Solution of the Non Synchronous Vibration in the AS900 Engine
 
2002-01-3007
Tail Icing Effects on the Aerodynamic Performance of a Business Jet Aircraft
 
2002-01-2939
The Benefits of a Wire Integrity Program
 
2002-01-2970
The Efficacy of Using Synthetic Vision Terrain-Textured Images to Improve Pilot Situation Awareness
 
2002-01-3023
The GP7200 Engine – Power for the Airbus A380
 
2002-01-2971
Use of Enhanced Vision Sensors for Approach Hazard Detection
 
2002-01-2923
Use of Victrex® PEEK™ Thermoplastic to Drive New Designs, Processing Flexibility, and Cost Reduction in Aerospace Components
 
2002-01-3013
Utilization Life of Electronic Systems - Aging Avionics Usable Life and Wear-Out Issues
 
2002-01-2995
Vertical Drop Test of a Narrow-Body Transport Fuselage Section with Overhead Stowage Bins
 
2002-01-2997
Vertical Drop Test of a Transport Fuselage Section
 
2002-01-2912
Wind-Tunnel Investigation of Commercial Transport Aircraft Aerodynamics at Extreme Flight Conditions
 
2002-01-3210
A Configurable Solid State Power Management and Distribution System
 
2002-01-3205
A Detailed Synchronous Machine Model
 
2002-01-3190
A Distributed Heterogeneous Simulation of a Representative Aircraft Power System
 
2002-01-3197
A Reciprocating-Mechanism Driven Heat Loop for High Heat-Flux Thermal Management
 
2002-01-3226
Active vs. Passive Means of Power Quality Improvement in Aerospace Applications
 
2002-01-3228
Aerospace DC Arcing Fault Detection Using Neural Network Techniques
 
2002-01-3175
Analysis and Simulation of a UAV Power System
 
2002-01-3219
Analysis of Fuel Cell/Battery– Capacitor Hybrid Sources Used for Pulsed Load Applications
 
2002-01-3182
Analysis of Switched Capacitive Machines for Aerospace Applications
 
2002-01-3233
Arc Fault Circuit Interrupter Development Overview
 
2002-01-3204
Arc Fault Diagnostics in Aircraft Electrical Systems
 
2002-01-3215
Bipolar Nickel Metal Hydride Batteries for Aircraft Applications
 
2002-01-3232
Closed-Form Frequency Model of 3-Phase Inverter Drive for DC Distribution System Analysis
 
2002-01-3214
Commercial Aircraft Batteries
 
2002-01-3180
Compact Pulsed Power Sources
 
2002-01-3183
Comparison of Pulse Width Modulation (PWM) Techniques for Advanced Aerospace Load Power Management Applications
 
2002-01-3216
Compatibility Testing and Smart Monitoring of the Hawker Battery on the ELDEC (Boeing) Chargers
 
2002-01-3229
DC Bus Regulation with a Flywheel Energy Storage System
 
2002-01-3243
Design and Endurance of Batteries with High Power/Energy
PT-133  
2002-01-3186
Design and Integration of DC Power System with Regulated Transformer Rectifiers
 
2002-01-3241
Design and Testing of the Mars Exploration Rover Lithium Ion Batteries
 
2002-01-3223
Design of a Piezoelectric Sensor-Based Controller for Mitigation of Torque Ripple in a Brushless DC Machine
 
2002-01-3212
Development of a Direct Drive Hall Effect Thruster System
 
2002-01-3244
Development of a Smart Secondary Microscopic Battery
 
2002-01-3238
Development of a Testbed for Design and Evaluation of Power Electronic Based Systems
 
2002-01-3195
Enhancement of Droplet Heat Transfer Using Dissolved Gases
 
2002-01-3231
Evaluation of Feature Extraction Technique for DC Arcing Fault at Aerospace Power Management and Distribution (PMAD) System
 
2002-01-3259
Field Results of Battery Management Technology Integration into a Vehicle Application (inGEN®)
 
2002-01-3198
Heat Transfer Characteristics of Evaporative Spray Cooling In a Closed Loop
 
2002-01-3260
High Density, High Performance Modular DC-DC Power Converter
 
2002-01-3196
High Heat Flux, Gravity-Independent, Two-Phase Heat Exchangers for Spacecraft Thermal Management
 
2002-01-3178
High Power and High Temperature Passive Application of CVD Diamond
 
2002-01-3253
High-Performance Sensorless PMSM Drive With Extended Kalman Filter
 
2002-01-3217
Implementation of New Aircraft Battery Technology in the Army
 
2002-01-3245
Lithiated Transition Metal Oxide Cathodes in Molten Nitrate Electrolytes for Lithium Thermal Batteries
 
2002-01-3240
Lithium Ion Batteries: Power Sources for Military Aircraft
 
2002-01-3187
Low-Weight, Low Cost AC/DC Converter for the V-22
 
2002-01-3200
Mass Advantages in a Jet-Pumped Active Thermal Management System
 
2002-01-3255
Modelling and Simulation Strategies for the Electric Systems of Large Passenger Aircraft
 
2002-01-3234
Multi-function, Bi-Directional and Compact Power Converters for Aircraft Power System Applications
 
2002-01-3185
Next Generation of Transformer Rectifier Units (TRU) with Full DC Voltage Regulation for Fixed and Rotary-wing Aircraft
 
2002-01-3207
Optimization of Launch Vehicle Energy Storage
 
2002-01-3213
Performance Tests of 22 Ah Metal Hydride Prismatic Design Cell Pack for Aircraft Applications
 
2002-01-3242
Performance Tests of a Developmental Lithium-ion Main Aircraft Battery
 
2002-01-3203
Polytopic Modeling and Lyapunov Stability Analysis of Power Electronics Systems
 
2002-01-3208
Power Magnetics Measurements, Modeling and Simulation
 
2002-01-3206
Power Quality Specification Development for More Electric Airplane Architectures
 
2002-01-3246
Pulse Power Nickel Metal Hydride Battery
 
2002-01-3181
Rapid Capacitor Charger for Compact Marx Generators
 
2002-01-3189
Real-Time Distributed Simulation of DC Zonal Electrical Distribution System
 
2002-01-3221
Ruthenium Oxide Super-Capacitor Performance Stability
 
2002-01-3191
Simulation of an Active Damping Device for DC Power Networks
 
2002-01-3184
Stability Analysis of a DC Power Electronics Based Distribution System
 
2002-01-3179
Study of High Energy Storage Blumlein Transmission Lines as High Power Microwave Drivers
 
2002-01-3236
The Development of an Electrical Wire Chafing Protective Technology for Aircraft
 
2002-01-3261
Thermal Design in Diode Array Packaging
 
2002-01-3230
Toward Intelligent PMAD Systems
 
2002-01-3254
Use of a High Inertia Motor with an Electric Actuator
 
2002-01-1267
NASA's Space Launch Initiative: A Program Overview
 
2001-01-3031
High Performance Executive Transport Design Employing Twin Oblique Lifting Surfaces
 
2000-01-3602
A Novel Charger/Discharger for the Parallel Connected Battery Module System
 
2000-01-3624
A Novel Start System for an Aircraft Auxiliary Power Unit
 
2000-01-3639
A Satellite Bus Power System
 
2000-01-3640
Advanced Electrical Power Distribution Network
 
2000-01-3623
Advantages of Spray Cooling for a Diode Laser Module
 
2000-01-3626
An Experimental Investigation into Turbine Trailing Edge Length Effect on Performance
 
2000-01-3649
An Observer-Based Automated Averaging Technique for Power Electronic Circuits
 
2000-01-3650
Automated Identification of the Operational Modes of Switched Electric Circuits
 
2000-01-3648
Average Value Modeling of Finite Inertia Power Systems with Harmonic Distortion
 
2000-01-3645
Behavioral Modeling of Batteries and Fuel Cells
 
2000-01-3628
Bipolar Metal Hydride Batteries for High Power and Aircraft Applications
 
2000-01-3590
Comparison of Vented Nickel Cadmium Aircraft Battery Technologies at Elevated Temperatures
 
2000-01-3603
Design and Implementation of a Digital Controller for DC-to-DC Power Converters
 
2000-01-3620
Design of a High Effectiveness Micro Exchanger for Mars Applications
 
2000-01-3652
Design of an Ultra High Power IGBT Inverter for Rapid Capacitor Charging
 
2000-01-3592
Development Of A Prototype Lithium Ion Battery for the F-16, F-18, and F-117 Aircraft
 
2000-01-3616
Directed Energy Switch: High Power Density, High Efficiency, High Temperature
 
2000-01-3644
Droplet Cooling Heat Transfer Model Validation
 
2000-01-3610
Energy Independence - Using Rechargeable Batteries in Wartime
 
2000-01-3647
Gas Turbine Dynamic Simulation Using Simulink®
 
2000-01-3601
High Power Density, High Efficiency, Low EMI DC to DC Converter for Space Applications
 
2000-01-3600
High Voltage Solid-Body Fuses for Use in Vacuum, Zero G, and Shock Environment
 
2000-01-3612
Induced Stirring at Lead Acid Battery Electrode Interfaces
 
2000-01-3604
Intelligent Systems for Power Management and Distribution
 
2000-01-3665
Magnetic Bearing Controls for a High Speed, High Power Switched Reluctance Machine (SRM) Starter/Generator
 
2000-01-3664
Mechatronic System Design Using a Multi-Domain Modeling Approach
 
2000-01-3621
Miniature Embedded Heat Pipes in Low Temperature Co-Fired Ceramic for Electronic Devices Requiring Temperature Stability
 
2000-01-3646
Modeling and Simulation of Power Electronics and Drives using MATLAB/Simulink
 
2000-01-3655
NDE Methodologies for Composite Flywheels Certification
 
2000-01-3622
Performance Characteristics of MOSFETs Operating at High Power
 
2000-01-3668
Performance Testing of Lithium-Ion Cells at JPL for Future NASA Aerospace Applications
 
2000-01-3613
Plastic Laminate Pulsed Power Development
 
2000-01-3636
Power Requirements for Future Robotic Space Missions
 
2000-01-3619
Power Supply and Energy Storage for Autonomous MEMS
 
2000-01-3635
Power and On-Board Propulsion System Benefit Studies at NASA GRC
 
2000-01-3608
Powering the Future Soldier
 
2000-01-3660
Primary and Regenerative Fuel Cells for UAV Applications
 
2000-01-3615
Proposed Microbattery/Laser Diode Application
 
2000-01-3593
Recent Developments and Trends in Aerospace Battery Maintenance, Charging and Analysis
 
2000-01-3625
Reducing Battery Maintenance Intervals
 
2000-01-3611
SAFT Lithium-Ion Polymer Battery Technology
 
2000-01-3641
SSP Power Management and Distribution
 
2000-01-3653
Sputtered Barium Titanate, Lead Zirconate Titanate, Barium Strontium Titanate Films for Capacitor Applications
 
2000-01-3617
Studies On A Helical Magnetic Flux Compression Generator
 
2000-01-3631
System Modeling of Advanced Electric Power Distribution Architectures for Large Aircraft
 
2000-01-3627
The International Electrotechnical Commission (Iec) and Aerospace Batteries
 
2000-01-3659
Tracking the Polar Principal Axis for Magnetic Bearing Control and Flywheel Balancing
 
2000-01-3638
V-22 Electrical Power System
 
2000-01-5560
A Method for Concept Exploration of Hypersonic Vehicles in the Presence of Open & Evolving Requirements
 
2000-01-5605
A Two Stage-to-Orbit High Staging Mach Number Design Concept
 
2000-01-5546
Aircraft Design Optimizing Operators, Environmental System and Manufacturers Requirements
 
2000-01-5602
An Early TSTO Fully Reusable Vehicle Design Used to “Calibrate” Stage 1 Combined-Cycle Hypersonic Propulsion Systems
 
2000-01-5559
Formulation, Realization, and Demonstration of a Process to Generate Aerodynamic Metamodels for Hypersonic Cruise Vehicle Design
 
2000-01-5561
Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter
 
2000-01-5618
Methodology for the Parametric Structural Conceptual Design of Hypersonic Vehicles
 
2000-01-5505
Military Pilot Training Concepts
 
2000-01-5503
Next Generation European Air System
 
2000-01-5547
Regional Aircraft Family Design
 
2000-01-5549
Research Programs for Transport Aircraft in Europe
 
2000-01-5507
The Sunriser - A Design study in Solar Powered Flight
 
1999-01-5583
Diesel Aircraft Engines: A Delayed Promise from the 1930’s
 
1999-01-5584
A Perspective on the First Century of Vertical Flight
 
1999-01-5644
Advanced Flying Automobile LS1 Engine
 
1999-01-1378
Next Generation Aircraft Auxiliary Power Systems
 
1999-01-1356
The Heat Pump Thermal Bus - An Alternative to Pumped Coolant Loops
 
1999-01-1359
VGCF/Carbon Composites for Thermal Management
 
985597
Barrel Aircraft Engines: Historical Anomaly or Stymied Innovation?
 
985556
High Stability Engine Control (HISTEC): Flight Demonstration Results
 
985526
Synerjet Powered Spaceliner: Aircraft Operability and Economics “Without Wings and Wheels”
 
981277
Technology Related to the Highly Maneuverable Lethal Vehicle (HMLV) Concept
 
972603
Advances in Commercial Engine Lube Debris Monitoring
 
972601
Development of a Two-Coat Non-Chromate Aluminized Epoxy
 
972604
Engine Management - Where do we go from here
 
972606
The Proposed FAA Organization Delegation Authorization System
 
971464
Avgas/Ethanol Dual-Fuel Aircraft Engine/Conversion
 
971485
Benefits Derived from Tracking Engine Performance of Flight Inspection Aircraft
 
962250
Jet Efflux Characteristics and their Influence on STOVL Aircraft Propulsion-Induced Effects
 
965525
High Power Induction Motor for Aircraft Spoiler
 
921039
The Application of Human Factors Engineering at General Electric Aircraft Engines
 
872348
Impact of Bypass Ratio on Thrust-to-Weight for V/STOL
 
872314
Performance Flight Testing of a Single Engine Powered Lift Aircraft
 
871012
Automotive Gasoline Usage in Reciprocating Aircraft Engines
 
860708
The Need for “Repeatability” in an Engineering Approach to Electrochemical Metallizing for Aircraft Applications
 
851839
The STOL Performance of a Two-Engine, USB Powered-Lift Aircraft with Cross-Shafted Fans
 
830772
An Experimental Investigation of Separated Flow on a Light Twin Engine Aircraft
 
830008
The Thunder Aluminum 390 Alloy Aircraft Engine
 
820614
Automatic Equipment for Spraying Aircraft Engine Parts
 
810849
A History of Aircraft Piston Engine Lubricants
 
801141
A Comparison of Propulsion Systems for V/STOL Supersonic Combat Aircraft
 
801156
Developing a Fighter Engine Derivative of the B-1/F101 Engine
 
770465
A Computer Technique for the Determination of Brake Horsepower Output of Normally-Aspirated Reciprocating Aircraft Engines
 
770466
Automotive Engines-A Viable Alternative for Aircraft
 
770488
High Fuel Economy in an Aircraft Piston Engine When Operating Ultralean
 
750505
AIRCRAFT ENGINE LUBE OIL FILTRATION STUDY
 
750629
The NASA Research Program on Propulsion for Supersonic Cruise Aircraft
 
751104
Three-Engine Two-Fan Navy Multimission V/STOL Aircraft Considerations
 
740473
A Study of High Temperature Fuels and Lubricants on Supersonic Aircraft/Engine System Performance
 
740382
Fuel System Requirements for Light Aircraft Turbocharged Reciprocating Engines
 
740383
Mathematical Simulation of a Vibrating Light Aircraft Piston Engine and Correlation with Engine Flight Test Data
 
720600
Aircraft Engines - A Vanguard of Air Transportation Progress
 
720315
Weather Radar for Single Engine Aircraft
 
710371
Aircraft Carburetor Icing Studies
 
710447
Design Integration The Key To Effective Engine Condition Monitoring
 
710470
Prop-Fan - A High Thrust, Low Noise Propulsor
 
710461
Why Maximum Temperature?
 
700235
A Fixed Base Engineering Flight Simulator for General Aviation Aircraft
 
700272
Consideration of Performance and Cost in Future Military Aircraft Engines
 
700268
Military/Commercial Aircraft Propulsion Relationships
 
700258
Morphology of Deposits in Aircraft and Engine Fuel Systems
 
700211
Starting Aircraft Engines with the Nickel Cadmium Battery
 
700290
Testing Results of Comprehensive Program for High Bypass Aircraft Engines
 
700205
Tiara Light Aircraft Engines - A New Generation
 
690403
Control Concepts for a High Bypass Aircraft Turbofan Engine
 
690425
Evolution of the Pratt & Whitney Aircraft JT9D Engine Oil System
 
690308
Functional Compatibility Analysis of Aircraft - Engine Fuel Systems
 
690653
INSTALLED PERFORMANCE OF THE TF39 ENGINE
 
690436
Ignition of Aircraft Fluids on High Temperature Engine Surfaces
 
680712
Performance Matching of the Propulsion System
 
680288
Airframe-Propulsion Integration for Future Aircraft Systems
 
680287
Integration of Inlet and Engine — An Airplane Man’s Point of View
 
680277
New Generation Engines - The Military Outlook for Adaptive Propulsion Systems
 
680279
New Generation Engines — Research Problems and Outlook
 
680294
Optimizing Exhaust — Nozzle/Airframe Thrust Minus Drag
 
680312
Aircraft Auxiliary Power Supplies
 
680229
Applications of Automotive Electrical Equipment to Light Aircraft Engines
 
680333
C-5A Propulsion System Installation
 
680337
Design Features for Maintainability in the Pratt and Whitney Aircraft J9D Gas Turbine Engine
 
680057
Designing for V/L Performance in an Aircraft Engine Fuel Pump
 
680644
Low-Speed Characteristics of High-Performance Lift-Engine V/STOL Aircraft
 
680317
Lubricants for Inerted Lubrication Systems in Engines for Advanced Aircraft
 
680226
Performance Characteristics of Aircraft with Turbosupercharged Engine and Cabin — 1968
 
680346
Smoke Measurement Techniques
 
680058
Structural Requirements for Aircraft Engine Main Fuel Pumps and Controls
 
670693
Applications of the ST6 Gas Turbine Engine
 
670138
An Approach to Simpler Control Requirements
 
670234
Designing Business Jet Aircraft Engines for Increased Service Life
 
670267
Powerplant Pressurization for Altitude
 
670248
Present Day Lubricants for Utility Aircraft Engines
 
670239
Professional Growth of Engineers with Business Aircraft Manufacturers
 
670249
The Cold Starting and Service Test Evaluation of an SAE 10W30 Aircraft Engine Oil
 
670237
The General Problems in Vibration of Aircraft Powerplant Components
 
670194
The Rotating Combustion Engine - Compact, Lightweight Power for Aircraft
 
670333
The Use of Composite Materials in Aero Engines
 
670238
Two-Stroke Light-Aircraft Engine Potential
 
660221
The Application of the High Bypass Turbofan for Business and Executive Aircraft
 
650265
A Method for Comparing and Selecting Propulsion Systems for V/STOL Aircraft
 
650377
Accurate Power Checking of Production Aircraft Engines
 
650839
Higher Propulsive Efficiency in Subsonic Aircraft
 
650831
LIFT FAN PROPULSION SYSTEMS V/STOL AIRCRAFT CONTROL
 
650201
Lift Engine Technology
 
650381
The Design and Development of the CJ610 Turbojet and the CF700 Turbofan Engines for Use in Business Jet Aircraft
 
650380
Turbocharging Aircraft Engine and Cabin
 
640209
Adaptation of Army Engine Inspection Techniques by Computer for Aircraft Applications
 
640236
An Approach to the Evaluation of Propulsion Systems in V/STOL Aircraft
 
640343
Analysis of Propulsion Systems for V/STOL Aircraft
 
640430
COMPONENT DEVELOPMENT OF A LIQUID METAL COUPLED REGENERATOR SYSTEM FOR REGENERATOR AIRCRAFT ENGINES
 
640438
Centerline Thrust for Twin Engine Aircraft
 
640344
Needed Research and Development on V/STOL Powerplants for Navy Aircraft
 
640059
New Test Procedures for Aircraft Piston Engine Oils
 
640440
Operation and Maintenance of the Flat Opposed Reciprocating Aircraft Engine as Related to Service Problems
 
640429
Test of a Regenerative Turboprop Aircraft Engine
 
640235
The Effect of Propulsion System Parameters on Vertical Take-Off and Landing Performance of a Transport Aircraft
 
640439
What Can Be Gained With Additive Oils in Utility Aircraft Engines
 
630039
Altitude Performance with Turbosupercharged Light Aircraft Engines
 
630036
Applications and Engineering Problems of VTOL - STOL Military Aircraft
 
630260
Breakerless High Frequency Ignition Systems for Reciprocating Aircraft Engines
 
630074
CONSIDERATIONS OF LIFT ENGINE INSTALLATIONS IN VTOL AIRCRAFT FROM THE VIEWPOINT OF THE AIRFRAME DESIGNER
 
630492
Evaluation and Test of a Liquid Metal Coupled Regenerator System for Aircraft Turboshaft Engines
 
630081
Powerplant system for V/STOL aircraft
 
620308
Extensions of the Lift/Thrust Engine Principle in V/STOL Aircraft
 
620300
Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft
 
620338
Recuperators for Long Duration Aircraft Engines
 
610342
A Consideration of Powerplants for Supersonic Transport Aircraft
 
610323
Lift-Thrust Turbofan Engines for VTOL and STOL Aircraft
 
600427
AN EVALUATION OF THE RELATIONSHIP BETWEEN RELIABILITY, OVERHAUL PERIODICITY, AND ECONOMICS IN THE CASE OF AIRCRAFT ENGINES
 
600290
CHOICE OF ENGINE TYPE FOR NUCLEAR POWERED MULTI-PURPOSE AIRCRAFT
 
600381
DEVELOPMENT OF IN-FLIGHT MODULATING TYPE THRUST REVERSER FOR SINGLE ENGINE AIRCRAFT
 
600265
TRENDS IN VTOL AIRCRAFT PROPULSION SYSTEM REQUIREMENTS
 
590289
A PROPULSION SPECTRUM FOR VTOL AIRCRAFT
 
590252
PYROPHORICS FOR AIRCRAFT PROPULSION THEIR PROMISE AND PROBLEMS
 
590261
SOME VIEWS ON AIRCRAFT NUCLEAR PROPULSION
 
590349
THE JT12 PRATT & WHITNEY AIRCRAFT'S 3000 LB. THRUST TURBOJET ENGINE
 
590047
selection of Optimum Modes of Control for aircraft engines
 
580076
DEVELOPMENTS IN THE FIELD OF DIRECT-AIR-CICLE ARICRAFT NUCRAFT NUCLEAR PROPULSION SYSTEMS
 
580070
JET ENGINE CONTROL AND ATTITUDE CONTROL IN VERTICAL ATTITUDE VTOL AIRCRAFT
 
580120
NEW FUELS FOR PISTON-ENGINE AIRCRAFT
 
570233
A DISCUSSION OF SOME RECENT DEVELOPMENTS IN AIRCRAFT ENGINE OIL FILTRATION
 
570020
COMPRESSOR STALL PROBLEMS IN GAS-TURBINE-TYPE AIRCRAFT ENGINES
 
570232
CONTAMINANTS AND THEIR EFFECTS ON AIRCRAFT ENGINES
 
570190
POTENTIAL ADVANCEMENTS IN THE FIELD OF SMALL AIRCRAFT ENGINES
 
570008
PREIGNITION IN AIRCRAFT RECIPROCATING ENGINES
 
560191
ACCELERATED SERVICE TESTING OF TURBO-PROP ENGINES IN USAF TEST BED AIRCRAFT
 
560270
ENGINE INLET AIR DIFFUSER CONTROLS FOR SUPERSONIC AIRCRAFT
 
550077
AIRCRAFT POWERPLANTS - PRESENT AND FUTURE
 
550239
Napier Nomad Aircraft Diesel Engine
 
550075
THE ALLISON T56 TURBO-PROP AIRCRAFT ENGINE
 
550078
TURBOJET ENGINES FOR PILOTLESS AIRCRAFT, PRESENT AND FUTURE
 
540199
A SYSTEMATIC SERIES OF ENGINES FOR UTILITY AIRCRAFT
 
540027
SIMULATED ALTITUDE TESTS OF LARGE AIRCRAFT ENGINE EXHAUST SYSTEMS
 
530001
THE STORY OF THE FIRST 50 YEARS OF AIRCRAFT ENGINES
 
530266
TITANIUM ALLOYS FOR AIRCRAFT ENGINE FORGINGS
 
520269
APPLICATION OF TITANIUM TO AIRCRAFT ENGINES
 
520224
Low-Temperature Lubrication of Aircraft Engines
 
520196
THE DEVELOPMENT OF RUST PREVENTIVE LUBRICATING OILS FOR RECIPROCATING AIRCRAFT ENGINES
 
510094
AN INTRODUCTION TO THE AIRCRAFT TURBO-JET ENGINE
 
510074
APPLICATIONS OF CERAMIC COATINGS IN AIRCRAFT ENGINES
 
510153
Airline Experience With Aircraft Engine Lubricating Oils
 
510167
Local Service Aircraft And Engine Maintenance Requirements
 
510151
Operational Experience With Multi-Engine Jet Aircraft
 
500167
Compound Engine Systems for Aircraft
 
500019
Driving Aircraft Accessories Remotely From The Aircraft Engine
 
500009
Fatigue Life Of Aircraft Engine Mounting Components
 
500151
Fuel And Lubricant Requirement Of Personal Plane Aircraft Engines
 
500072
Investigation Of Reversing Propeller Pitch On A Multi-Engine Aircraft In-Flight
 
500153
Light Aircraft Engine Tests--Fuels And Operating Variables
 
490173
ATOMIC POWER And Aircraft Propulsion
 
490071
Fuel Systems And Carburetors For Personal Aircraft
 
490232
LUBRICATION, FRICTION AND WEAR STUDIES WITH HIGH-OUTPUT AIRCRAFT ENGINES
 
480142
A Method Of Evaluating Aircraft Engine Oils By Piston Ring Sticking Tests
 
480100
Engineering Developments Required For Satisfactory Low Temperature Aircraft Engine Operations (Extract)
 
480179
INSTRUMENTATION for Development of AIRCRAFT POWERPLANT COMPONENTS Involving FLUID FLOW
 
480221
PREIGNITION And Its Deleterious Effects in Aircraft Engines
 
480048
The Design And Development Of Rocket Engine Powerplants For Aircraft
 
470030
Aircraft Engine Starters
 
470218
Aircraft-Engine Starting Tests and Experiences in the Arctic
 
470016
DESIGN TRENDS IN TURBO-JET AND TURBO-PROP AIRCRAFT ENGINES
 
470153
Engines For Light Aircraft
 
470117
Evaluation Of Light Aircraft Engine Lubricants
 
470076
Experiments With Converted Automotive Engines For Light Aircraft Power Plants
 
470240
FUTURE TRENDS IN AIRCRAFT-ENGINE DESIGN
 
470156
Installation Engineering Of Aircraft Turbo-Jet Engines
 
470214
Mutual Adaptation of Aircraft Fuels and Engines
 
470239
Predicted Effects of the Atmosphere on Turbine-Type Aircraft Engines
 
470053
Rocket Engines as Applied to Future Aircraft Powerplants
 
470193
Transport Aircraft Powerplant Outlook For 1947
 
460195
A PETROLEUM ENGINEER LOOKS at AIRCRAFT FUELS
 
460122
Aircraft Engine Induction System Deposits
 
460143
DEVELOPMENT OF CHROME PLATED PISTON RINGS FOR AIRCRAFT ENGINES
 
460243
FUEL SENSITIVITY and ENGINE SEVERITY in Aircraft Engines
 
460205
Factors Pertaining to Installation of Inverted, In-Line AIRCOOLED AIRCRAFT ENGINES
 
460209
Factors in AERATION and DEAERATION of AIRCRAFT-ENGINE OIL
 
460035
Investigation of an Opposed Piston Light Aircraft Engine
 
460061
NACA Study of the Utilization of Exhaust Gas of Aircraft Engines
 
460121
The Two Cycle Engine In Aircraft The Crankcase Scavenge Target Engine
 
460259
Utilization of Exhaust Gas of Aircraft Engines
 
460192
WATER INJECTION for Aircraft Engines
 
460110
“Liquid Cooled Engine Power Plants for Transport Aircraft”
 
450236
AXIAL vs CENTRIFUGAL SUPERCHARGERS for Aircraft Engines
 
450213
Aircraft-Engine GEARS
 
450056
BOND TESTING OF SILVER PLATED AIRCRAFT ENGINE PARTS
 
450229
DETECTION of DETONATION and Other Operating Abnormalities in AIRCRAFT ENGINES by Means of Special Instrumentation
 
450155
DIFFICULTIES with ENGINES INSTALLED in CIVIL AIRCRAFT
 
450178
Fuel Injection for the Aircraft Engine
 
450237
High - Conductivity Cooling Fins for Aircraft Engines
 
450163
Late Developments of the Allison Aircraft Engine
 
450158
Lessons from Aircraft Engines Applied to Heavy-Duty Ground Vehicle Engines
 
450139
S-S System of Lubrication for Aircraft Engines
 
450012
THE DETECTION OF DETONATION AND OTHER OPERATING ABNORMALITIES IN AIRCRAFT ENGINES BY MEANS OF SPECIAL INSTRUMENTATION
 
450118
“SERVICE EXPERIENCE WITH LIGHT AIRCRAFT ENGINES”
 
440032
AIRCRAFT ENGINE CARBURETORS AND THEIR ACCEPTANCE TESTING
 
440037
AIRCRAFT ENGINE PRODUCTION AS VIEWED BY AN AUTOMOBILE MANUFACTURER
 
440039
AIRCRAFT ENGINES IN TANKS
 
440002
AIRCRAFT ENGINES, AND THEIR ACCESSORIES
 
440011
AIRCRAFT POWERPLANT DEVELOPMENT TESTING
 
440167
Aircraft-Engine - INLET and EXHAUST PORTING
 
440203
An Investigation of CHAFING on AIRCRAFT-ENGINE PARTS
 
440146
OPERATING TEMPERATURES and STRESSES of ALUMINUM AIRCRAFT-ENGINE PARTS …
 
440101
RADIO INTERFERENCE AND THE AIRCRAFT ENGINE
 
440175
SYNTHETIC RUBBER APPLICATIONS on Aircraft Engines
 
440201
Some Aircraft-Engine PRODUCTION METHODS
 
430149
CARBURETION for the AIRCRAFT ENGINE
 
430100
Corrosion preventive oil and aircraft engine preservation
 
430154
INTAKE SYSTEMS for AIRCRAFT ENGINES
 
430133
NEW MATERIALS for AIRCRAFT ENGINES
 
430130
Re-REFINING of Aircraft-Engine Oils
 
430118
Requirements for carburetor air filters for aircraft engines
 
430024
THE EFFECT OF ENVIRONMENT ON AIRCRAFT ENGINE DESIGN AND PERFORMANCE
 
430153
The POSSIBILITIES of SHAVED GEARS for AIRCRAFT ENGINES
 
420087
AIRCRAFT CARBURETOR AIRSCOOPS on FUEL-AIR and Their Effect METERING in Flight
 
420131
AIRCRAFT-ENGINE RADIO SHIELDING
 
420077
Cooling Characteristics of SUBMERGED LIGHT AIRCRAFT ENGINES
 
420123
Design Features of the JUNKERS 211B AIRCRAFT ENGINE
 
420126
Limiting Factors of OVERHAUL PERIODS for AIRCRAFT ENGINES
 
420098
The Automotive Body Engineer in AIRCRAFT
 
420074
“PROPELLER CONTROL and ITS RELATION to POWER in AIRCRAFT ENGINES”
 
410099
ALTITUDE PERFORMANCE of High-Output Aircraft Engines
 
410089
Aircraft-Engine REDUCTION GEARS and TORQUE METERS
 
410138
Design of AIRSCOOPS for AIRCRAFT CARBURETORS
 
410110
Engineering Considerations in the Application of AUTOMOBILE METHODS to AIRCRAFT PRODUCTION
 
410131
MERCEDES-BENZ DB-601A AIRCRAFT ENGINE - (Design Features and Performance Characteristics)
 
410001
MODERN AIRCRAFT ENGINE TESTING
 
410007
MORE AIRCRAFT ENGINES FOR NATIONAL DEFENSE
 
410006
Some Factors Influencing Aircraft Engine-Propeller Vibrations
 
410118
Standardization of AIRCRAFT - ENGINE COMPONENTS
 
410137
The ALLISON AIRCRAFT-ENGINE DEVELOPMENT
 
400166
ALTITUDE and the Aircraft Engine
 
400126
Design Problems in the Quantity Production of Aircraft Engines
 
400133
High-Output Aircraft Engines
 
400137
Performance of Aircraft Spark-Ignition Engines with Fuel Injection
 
400147
Progress in Light Aircraft Engines
 
400041
SPECIAL PROBLEMS IN THE PRODUCTION OF AIRCRAFT ENGINES
 
390166
A Non-Icing Fully Maneuverable Aircraft Carburetor
 
390181
Aircraft Engines and Their Lubrication
 
390121
Aircraft-Engine Lubrication
 
390136
Aircraft-Engine Valve Mechanisms
 
390132
Coordinating Aircraft-Engine Design and Production
 
390050
DYNAFOCAL SUSPENSION FOR RADIAL AIRCRAFT ENGINES
 
390145
Dynamic suspension~A method of aircraft-engine mounting
 
390088
ENGINEERING EXPERIMENTAL AIRCRAFT
 
390151
Fuel-Economy Possibilities of Otto-Cycle Aircraft Engines
 
390160
Permissible Amplitudes of Torsional Vibration in Aircraft Engines
 
390157
Prospects for Use of “Safety Fuels” in Spark-Ignition Aircraft Engines
 
390185
Vibration Characteristics of Aircraft Engine-Propeller Systems
 
380111
BASIC PROBLEMS IN THE DESIGN OF HIGH-OUTPUT AIRCRAFT ENGINES
 
380143
Engine Installation and Related Problems in Large Aircraft
 
380152
Propeller Factors Tending to Limit Aircraft-Engine Powers
 
380177
Rating Aviation Fuels in Full-Scale Aircraft Engines - Completion of First Program and Progress on Second Program-Report of the Cooperative Fuel Research Committee
 
380140
The Accessory-Drive Problem of Aircraft Engines
 
380137
The Diesel as a High-Output Engine for Aircraft
 
380161
The Single Sleeve as a Valve Mechanism for the Aircraft Engine
 
380159
Torsional Vibration of In-Line Aircraft Engines
 
370035
AIRCRAFT ENGINE MAINTENANCE
 
370177
Aircraft Powerplant Trends
 
370153
Aircraft-Engine Installation Vibration Problems
 
370142
Aircraft-Engine Materials
 
370193
Design of Cowlings for Air-Cooled Aircraft Engines
 
370179
Features of the In-Line Air-Cooled Aircraft Engine
 
370150
High Output in Aircraft Engines
 
370161
Lubrication and Cooling Problems of Aircraft Engines
 
370145
Plant Layout and Production Methods for Modern Aircraft Engines
 
370129
Selections of Oils for High-Output Aircraft Engines
 
370171
The Determination of Ratings for Transport Aircraft Engines
 
360035
AIRCRAFT ENGINE PISTON RING AND CYLINDER WEAR
 
360132
Air-Cooled Radial Aircraft-Engine Installation
 
360121
Air-Cooled Radial Aircraft-Engine Performance Possibilities
 
360007
CYLINDER WEAR AND PISTON RING STICKING TENDENCIES OF AUTOMOBILE, BUS AND AIRCRAFT ENGINES
 
360105
Eliminating Crankshaft Torsional Vibration in Radial Aircraft Engines
 
360127
Future Possibilities of 100-Octane Aircraft-Engine Fuel
 
360070
NAVAL AIRCRAFT ENGINES
 
360112
Rating Aviation Fuels-in Full-Scale Aircraft Engines - A report of the Cooperative Fuel Research Committee
 
360049
Some Recent Developments in Aircraft Engines
 
350112
Aircraft Spark-Ignition Versus Compression-Ignition Engines
 
350107
An Automatic Power and Mixture Control for Aircraft Engines
 
350119
An analysis of critical stresses in aircraft-engine parts
 
350086
Fuel Injection as Applied to Aircraft Engines
 
350113
Further Progress in Controlled Cooling of Radial Aircraft Engines
 
350076
MODERN AIRCRAFT ENGINE DEVELOPMENTS
 
350097
The Influence of Engine Oils on Aircraft-Engine Performance
 
340096
Altitude Performance of Aircraft Engines Equipped with Gear-Driven Superchargers
 
340018
Design Limitations of Aircraft Engines
 
340116
Ice Formation in Aircraft-Engine Carburetors
 
340089
The Cowling and Cooling of Radial Air-Cooled Aircraft Engines
 
320069
Bending Moments in the Master Rod of a Radial Aircraft Engine
 
320012
Indicators as a Means of Improving Aircraft-Engine Performance
 
320037
Magnesium Alloys in Aircraft-Engine Construction
 
310040
Bearing-Load Analysis and Permissible Loads as Affected by Lubrication in Aircraft Engines
 
300037
Aircraft-Engine Installation
 
300024
Fuel Requirements of the Gasoline Aircraft-Engine
 
300023
Gasoline Requirements of Commercial Aircraft Engines
 
300034
THE PACKARD DIESEL AIRCRAFT-ENGINE
 
290057
Diesel Engines for Aircraft
 
290063
Modern Light Alloys and Their Application to Aircraft-Engine Design
 
280064
The Packard X 24-Cylinder 1500-Hp. Water-Cooled Aircraft Engine
 
270027
Recent Development in Aircraft Powerplants
 
260064
A ROOTS-TYPE AIRCRAFT-ENGINE SUPERCHARGER
 
260060
AIR-COOLED ENGINES IN NAVAL AIRCRAFT
 
260063
PROGRESS IN AIRCRAFT-ENGINE DESIGN
 
260061
THE DEVELOPMENT OF THE WRIGHT WHIRLWIND TYPE J-5 AIRCRAFT-ENGINE
 
250066
SOME ASPECTS OF AIRCRAFT-ENGINE DEVELOPMENT
 
240033
EXHAUST-VALVES AND GUIDES FOR AIRCRAFT ENGINES
 
230011
AIRCRAFT-ENGINE PRACTICE AS APPLIED TO PASSENGER-CARS
 
230028
RECENT DEVELOPMENTS IN AIRCRAFT ENGINES IN THE NAVY1
 
220030
RECENT AIRCRAFT ENGINE DEVELOPMENTS
 
190005
Possible effect of aircraft engine development on automobile practice
 
190020
THE LIBERTY AIRCRAFT ENGINE
 
180050
THE HISPANO-SUIZA AIRCRAFT ENGINE
 

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