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SAE International

SAE Papers

Paper Number Paper Title Book Number
2008-01-2874 Small Turbine Engine Evolution V117-2008
2-28-4-26 Clean, quiet commercial propulsion
2-28-2-30 Narrowing in on military requirements
2-27-10-20 Older-older vs. newer-older: room for both
2-27-9-33 Creating, customizing aircraft interiors
2-27-8-16 Sound sound-research techniques
2-27-3-22 Transatlantic testing program for the F-35
2-27-1-16 On-wing designs
2-25-10-16 All Things to All Operators
2-26-6-30 Better seen, not heard
2-26-3-14 Full throttle for engine solutions
2-26-1-22 Maintaining Reliability
2-25-3-18 Stovl Propulsion--Onward and Upward
2-26-3-19 To the breaking point
2-24-10-24 Distributed Simulation
2-24-9-23 Propelling Commercial Aircraft
2-24-4-29 Speeding Up Engine Manufacture
2-23-6-25 Fire-Resistant Composites for Engine Nacelles
982869 In-Flight Thrust Determination
971249 The Engineering Challenge-To Retain Technical Excellence in the Changing Aerospace Environment
942106 Air Turbine Start System for the Next Generation of Large Commercial Aerospace Engines
942141 Computational Support to Engine Test
942103 Design Improvements and Their Evaluation in Pneumatic Starters for Gas Turbine Engines
942104 Enhanced Air Turbine Starter Clutch Design
942140 Pw4084 Engine Testing in Altitude and Sea Level Test Facilities
942105 Synchronous Engagement Clutch
941172 Benefits Obtained Using Ai Based Test Equipment on Installed Turbine Engines
941150 Engine Life Measurement and Diagnostics; the Future Direction for the Air Force
941175 Enhancing System Availability and Performance in Combined Cycle Power Plants By the Use of Condition Monitoring
941151 In Operation Detection and Correction of Rotor Imbalance in Jet Engines Using Active Vibration Control
940053 Chemical Removal of Ceramic Thermal Barrier and Metallic Bond Coats From Gas Turbine Combustion Components
932633 Health Evaluation of Turbine Engines Undergoing Automated FAA Type Cyclic Testing
931449 Dynamic Stiffness and Damping of Foil Bearings for Gas Turbine Engines
931444 Lightweight High-Temperature Fuel Metering Valves
931442 Lightweight, Opto-Electronic Engine Control System for Aerospace Turbine Engines
921976 Accumulated Thermal Damage Analysis of Synthetic Turbine Engine Oils
921955 Gyroscopic Test for the T800-Lht-800 Turboshaft Engine
921974 Switched Reluctance Starter/Generator
921975 Trends in Air Turbine Starters for Large Turbofan Engines
912029 A Calculation of Penetration of the Jet Issuing Normally Into a Cross Flow Across a Wall Boundary Layer
912032 A Simplified-Model Approach to Group Combustion of Fuel Spray
911167 Case Studies: Keys to Success in Laser Processing Aircraft and Turbine Engine Parts
911207 The Impact of Advanced Materials on Small Turbine Engines
902023 A High-Speed Fuel Lubricated Hybrid Thrust Bearing for Limited-Life Turbine Engines
901810 The Role of the Turbulent Prandtl Number in Turbine Blade Heat Transfer Prediction
901064 Development Study on Expander Cycle Air Turbo-Ramjet With Intake Air Cooler for Space Plane
892254 Fast Start Ceramic Auxiliary Power Unit
892251 Garrett Multipurpose Small Power Unit (Mpspu)--Program Status 1989
881499 Pneumatic Link Secondary Power Systems for Military Aircraft
881501 T-100 Multipurpose Small Power Unit--Technology for the Next Generation Auxiliary Power Units
881551 Turbine Technology-Materials Set the Pace
861706 Borescope Inspection Training and Certification
861712 Fast Start Apu Technology
861711 Past, Present and Future of Hydraulic Apu Start Systems
851881 Harrier Iii-Av8b With a Modern Engine
851785 Effects of Section Thickness and Orientation on Creep-Rupture Properties of Two Advanced Single Crystal Alloys
851994 Evaluation of Jftot Tube Deposits By Carbon Burnoff
851798 Performance Advantages of High Load Aviation Lubricants
851787 Processing Study of Injection Molding of Silicon Nitride for Engine Applications
851829 Reliability and Maintainability--A Look At the Rolls-Royce Rb.211
851799 Some Aspects of Fluorocarbon Elastomer Compatibility With Gas Turbine Lubricants
851882 The Significance of Advanced Technology Engines on V/Stol Systems
851995 Whats Happening in Aircraft Engine Product Support
850901 Air-Cycle Air Conditioning of Turbine-Powered General Aviation and Commuter Aircraft
821374 Closed-Loop Engine Fuel System Simulation
821373 Hybrid Computer Simulation in Digital Fuel Control Design
821515 Production of P/M Near-Net Shape Superalloy Hardware
801124 A Forward Look At Gas Turbine Testing Facilities
801121 A Review of the Installation, Performance and Economic Aspects of a High Altitude Facility for Small Gas Turbines
801200 An Application of Redundancy in Digital Electronic Engine Control
801220 Commercial Ems Considerations for Small Gas Turbine Engines
801149 Development Requirements for Integrated Aircraft Power Systems
801201 Flight Test Reliability Demonstration of Electronic Engine Controls
801158 Fuel Efficiency Improvements to the T56 Turboprop Engine
801116 Improved Components for Engine Fuel Savings
801118 Performance Deterioration of Commercial High-Bypass Ratio Turbofan Engines
801151 The Status of the Expendable Gasifier Program
801231 Unistructure - a New Concept for Light Weight Integrally Stiffened Skin Structures
800617 Vibration Aspects of Small Turbine Engines in Aircraft Installations
791103 Aerospace Component Repair Procedures
781001 An Alternating Direction Explicit Method for Computing Three-Dimensional Viscous Flow Fields in Turbomachines
781003 An In-Place Recalibration Technique to Extend the Temperature Capability of Capacitance-Sensing, Rotor-Blade-Tip-Clearance Measurement Systems
781029 Life Cycle Cost in Advanced Technology Engine Development
781032 Life Cycle Cost in Preliminary Engine Design
780992 Planning the Development and Qualification Process for the Next Generation of High Technology Aircraft Engines
780990 Recent General Electric Engine Development Testing for Improved Service Life
780994 Requirements and Constraints in the Development and Qualification of Gas Turbine Engines for the Navy
780991 The Application of a Design Verification System and Accelerated Mission Testing to Gas Turbine Engine Development
781031 Turbine Engine Cost Reduction Using Life Cycle Cost Techniques
770961 A Microprocessor Based Sequencer for Gas Turbine Engines
771010 Advanced Supersonic Transport Propulsion Systems
770994 Condition Monitoring Experience on Cf6 Engines
770962 Design and Application of Programmable Sequencers to Gas Turbines
770968 Design of An Industrial Gas Turbine Intake--A Critical Item
770993 Gas Path Analysis Applied to Pre and Post Overhaul Testing of Jt9d Turbofan Engine
770992 Gas Turbine Module Performance Analysis
770991 Modular Engine Maintenance Concept Considerations for Aircraft Turbine Engines
770974 Transient Expansion of the Components of An Air Seal on a Gas Turbine Disc
770976 Turbine Engine Slip Ring Technology - a Survey
760926 Air Force Facility for Large Turbine Engine Compressor Testing
760919 Fuel Additives to Inhibit Sulfidation
760908 Silencing Experience With a Large Gas Turbine
760925 The Use of Vortex Generators as Inexpensive Compressor Casing Treatment
751070 Applying Resilient Foil Air Bearings to Turbomachinery -- Techniques and Challenges
751061 Electronic Fuel Controls for Missile and Rpv Gas Turbines
751072 Evaluation of a Gas-Lubricated Foil Bearing for Control of Gas Turbine Engine Rotor Critical Speeds
751064 Evolution of An Electronic Fuel Control for Industrial Gas Turbines
751047 Progress Report on the GatorizingUtUm Forging Process
751049 Rene 125, Development and Application
751050 Trends in High Temperature Materials Technology for Advanced Aircraft Turbine Engines
740806 Altitude Evaluation of a Variable Cycle Turbofan Engine
740846 Design and Development of a Gas Turbine Powered Silent Power Package
740865 Implications of Multiplane-Multispeed Balancing for Future Turbine Engine Design and Cost
740807 Larzac: a Small Turbofan Engine for Military and General Aviation Aircraft
740847 Maintenance Considerations in Aircraft-Derivative Industrial Gas Turbines
740849 Performance Development History -- 10 Kw Turboalternator
740848 The Transition From Effective Aircraft Engine Control to Effective Industrial Engine Control
730880 Aerospace Fluidics Applications and Circuit Manufacture
730909 An Approach Toward Optimizing Material Cost and Part Function in Advanced Powerplants
730929 Production Acceptance Testing Using An Improved Acoustic Signature Analysis
730932 Vibration Monitoring of a 750 Kw Gas Turbine Generator
720826 Aero Engines for Navy Shipboard Use
720834 Design and Analysis of An Apu Monopropellant Gas Generator
720824 Development and Use of Aircraft Derivative Turbines in Industrial and Marine Applications
720827 Innovative Ideas in the Application and Wide Use of Small and Medium Size Industrial Gas Turbines
720836 Storable Fueled Power System for Space Shuttle
720825 The Industrial Jet Gas Turbine for Base Load Applications
710462 High-Temperature Aircraft Turbine Engine Design Considerations
700823 Control System Requirements and Considerations for High-Temperature Turbine Engines
700821 Direct-Drive Turbine Engine Control Components and Airframe Accessories Will Be Feasible By 1980
700826 Engine Control Concepts for the Augmented Turbofan
700814 Hamilton Standard Auxiliary Power Unit for Lockheed Tristar Airliner Utilizes Free-Turbine Engine
700825 Jet Engine Control Systems - Their Evolution, Future Requirements and Potential Limitations
700822 Microelectronic Circuits Can Be Selected and Tested to Meet Severe Temperature and Vibration Environment of Aircraft-Engine Controls
690424 Lubricant Evaluation and Systems Design for Aircraft Gas Turbine Engines
690332 On Board Gas Turbine Apus for Executive Aircraft
680447 Design Requirements of Small High-Temperature-Rise Combustors for Turbine Engines Designed for Vtol Aircraft
680310 Modular Accessory Concept for Turbine Engines in Military Aircraft
670888 Application of Fasteners to Large Aircraft Gas Turbine Engines
670552 Application of Fluidics to Control Systems of Ramjet Engines
670584 Computer Technique to Evaluate Routing of Tubing on Turbine Engine Fuel, Oil, and Hydraulic Systems
670332 Containment Evaluation Facility Has Been Built to Make Turbine Rotor Burst Containment a Reality
670344 Design Criteria and Configuration for Long-Life Aircraft Turbine Engines
670862 Development of Filament Reinforced Titanium Alloys
670366 Three Emulsified Fuels Are Tested in Turbine Combustors, Fuel Controls, Fuel System Component Parts, and in Three Turboprop Engines
670358 Turbine Engine Diagnostics Helps Airlines Avoid In-Flight Engine Failures
670968 United Aircraft Turbotrain Has Free Turbine Engine, Lightweight Structure and Banking Suspension to Allow High Speed Operation
660296 Airline Operational and Economic Goals of the Supersonic Transport Propulsion Systems
660313 Extended Engine Life Through In-Service Development
660073 Factors Influencing Aircraft Turbine Engine Oil Drain Practices
660310 Protective Coatings for Extended Life of Aircraft Jet Engine Parts
660634 Recent Advances in Forging Beryllium for Aerospace Applications
660333 United Aircraft Corp. Turbine Powered Train, With Emphasis on Its Suspension System
650841 Design and Operational Information on Components and Subsystems of Mach 3 B-70a Propulsion System
650814 Extension of Drain Periods in Gas Turbine Engines Using Improved Synthetic Lubricants
650826 Keeping the Boeing 727 Self-Sufficient--One Year of Service With An On-Board Auxiliary Power Unit
650816 Testing Mil-L-23699 Turbine Engine Luricants in the Ge J79 Jet Engine
640423 A lightweight universal fuel control for aircraft turbine engines
640611 Aircraft gas turbine engine trend analysis
640389 Bendix flameout sensor for turbine engine aircraft
640489 Consideration of the high bypass ratio tip turbine cruise fan for long range and long endurance aircraft
640805 The Aircraft Regenerative Turbine Engine-Where Now
630567 Trend analysis as applied to gas-turbine engines and aircraft mechanical equipment
620057 Gas turbines and the business aircraft
620054 The trend to turbines in business aircraft
610367 Industrial power requirements and the aircraft gas turbine engine
610358 Turbine powered transport aircraft in the USSR
580169 Developments in aircraft turbine lubricants
580170 Relation of fuels to aircraft turbine engines
580069 The turbonator~An integrated air turbine generator for high mach aircraft
570200 Developments in aircraft turbine lubricants
560171 Dynamic seals for aircraft gas turbine engines
560293 General fuel requirements for the commercial aircraft gas turbine engine
550014 Bearings and lubricants for aircraft turbine engines
540085 Inlet protection for aircraft gas turbine engines
540084 Retractable air inlet screens for aircraft gas turbines
530177 Aircraft gas turbines
530013 Aircraft turbine engine synthetic lubricants and their lubricating properties
530258 Instrumentation for aircraft gas turbine development
530147 Small turbines~The heart of modern aircraft accessory power systems
520206 Characteristics and limitations of expansion turbines for auxiliary power purposes in turbine-propelled aircraft
520149 The case for turbines in small aircraft
510170 Flight experience with turbine propeller powered aircraft
510002 The development of the aircraft gas turbine in Great Britain and its influence on petroleum requirements
500176 Auxiliary gas turbines for pneumatic power in aircraft applications
490117 Sand and dust erosion in aircraft gas turbines
460150 Air conditioning of turbine-propelled military aircraft
460239 Aircraft gas turbines with centrifugal compressors
460113 Automatic control considerations for aircraft gas turbine propeller power plants
460237 Gas turbines and aircraft

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