SAE Papers

Paper Number	Paper Title	Book Number
2008-01-2232	Operational Loads Monitoring of a Fleet of Beech 1900D Aircraft	V117-2008
2008-01-2266	Outsourcing Aircraft Maintenance
2-27-4-18	Plain talk from plane engineers
2-23-3-18	Airflow Simulation for Winglets
2-21-10-29	737-800 Winglet Integration
2000-01-5585	Fasteners Modeling for Msc.Nastran Finite Element Analysis
2000-01-5586	Impact Simulation of Simplified Structural Models of Aircraft Fuselage
1999-01-5640	Development of Wing Structural Weight Equation for Active Areoelastic Wing Technology
1999-01-5594	Optimization of the Wing Structure of a Future Supersonic Transport Aircraft
1999-01-5572	Validating FAA Structural Loads Regulations Using Operational Data
981732	Radiator Wing Rotation Algorithm Overview for the International Space StationS External Active Thermal Control System
985601	Wing Manufacturing: Next Generation
975605	Application of Dimensional Management on 747 Fuselage
975604	Gd&T for Flexible Contoured Structures
972625	Aircraft Applications for the Controlled Shot Peening Process
972626	Damage Tolerance Assessment of Casa Landing Gear
972624	Incorporating Hole Cold Expansion to Meet Durability and Damage Tolerance Airworthiness Objectives
972622	Results From Faa Program to Validate Bonded Composite Doublers for Commercial Aviation Use
972623	The Role of D Sight in Military Aircraft Inspection
971460	System Component Coupling for Structure-Borne Noise Isolation Studies
961322	Phase Change Materials--Current Potential and Future Direction
961256	Thin Film Inerting Enclosure for Out of Chamber Weld Repair of Titanium Structures
951174	An Example of Low-Cost Structural Testing
951448	Automation Benefits for Starch Media Dry Stripping
942162	Aging of Polymeric Materials for Use on Hsct
941837	Automatic Riveting Cell for Commercial Airplane Floor Grid Assembly
941832	Automatic Stringer Drilling System (Asds)
941836	Gantry 5 Axis Dnc/Cnc High Speed Milling and Drilling Machine With Integrated Multiflexible Universal Holding Fixture for the Aerospace Industry
942161	Materials and Structures Trade Studies for the High-Speed Civil Transport
942158	Spf/Db Wing Structures Development for the High-Speed Civil Transport
941232	Considerations in the Service Life Extension Program for the C-141 Aircraft
931221	An Investigation of the Accuracy of Fem Analysis of a Graphite Epoxy Box Beam
931259	Corrosion Prevention and Control Programs for Boeing Airplanes
921461	Theoretic and Experimental Verification on the Efficiency of Crack Stopper in Pressurized Fuselage
922040	An Advanced Alloy for Landing Gear and Aircraft Structural Applications--AermetSr 100 Alloys
922400	Production and Repair of Fastened Joints Incorporating Cold Expansion
912233	Damage Tolerance Philosophy for Fiber/Metal Laminates
911984	The Fatigue Scatter Factors and Reduction Factors in the Design of Aircraft and HelicopterS Structural Lives
910934	A Method for On-Aircraft Anodizing: Phos-Anodizing Containment System
910928	An Environmentally Acceptable Paint Stripping System
910927	Test Procedure for Dense Particle Separator
902040	A Flexible Lateral Seam Riveting System for Circular Aircraft Structures
902047	Automated Installation of Delron Inserts in Aircraft Floor Boards
902038	Designed Experiments and Statistical Process Control for Automatic Fastener Installations
902036	Mini-Riveter Update/Applications
901938	Advanced Composite Use Experiences--The Basis for Future Applications
901066	Advanced Structures of Hypersonic Vehicles and Aerospace Planes
900997	Analysis and Certification of the Starship All-Composite Airframe
891058	Aerospace Structures Supportability
891042	Resin Transfer Molding of Composite Aircraft Structures
880976	Outsized Air Cargo--A New Approach to Shoring
872458	A Frequency Domain Mimo Modal Identification Method With Application in the Aircraft Ground Vibration Test
872419	Mission-Adaptive Wing
872325	Correlation of Entrainment and Lift Enhancement for a Two-Dimensional Propulsive Wing
871022	Certification of Bonded Composite Structure
860811	Three-Dimensional Traveling Load Finite Element
850893	Design and Use of KevlarSr in Aircraft Structures
850903	Designing Composites for Producibility
850863	Manufacturing Tolerances for Natural Laminar Flow Airframe Surfaces
850915	Usaf Damage Tolerance Methods Applied to General Aviation Aircraft Design and Analysis
850713	Abrasive Blast Cleaning--A Viable Alternative to Chemical Stripping Operations
850703	New Technology Bonding Corrosion Protection and Durability
850712	Paint Removal Through Plastic Bead Blasting--The Sensible Way
830768	Prediction of Aircraft Structural Damage From Acoustic Overpressures Due to Lightning Strikes
811303	Energy Absorption of Channel Beams During Gross Deformation
810467	Automated Lamination of Production Advanced Composite Aircraft Structures
800932	Effects of Stress on the Performance of Agricultural Equipment Operators
800879	Composites Structure Applications--Piper Cheyenne Iii
800612	Thermal Expansion Molding Process for Aircraft Composite Structures
790563	Adhesive Bonded Structure of New Pressurized Piston Twin Aircraft
790561	Bonding and Durability
790589	Experimental Verification of Program Krash--A Mathematical Model for General Aviation Structural Crash Dynamics
790612	Fretting Fatigue, With Reference to Aircraft Structures
790627	Summary of Noise Reduction Characteristics of Typical General Aviation Materials
770452	Simplified Methods for Determining Stresses and Deflections of Thin Laminated Composite Plates
760452	Fracture in Thin Sections
760451	Reduction of Pressure Survey Data With Regression Analysis
750511	Comparison of Fracture and Fatigue Properties of Clad 7075-T6 Aluminum in Monolithic and Laminated Forms
750531	Expanded Thermoplastic Core: a New Dimension in Plastics for Structural Applications
750533	Graphite Composite Materials Applications in Aircraft Structures
750517	Public Acceptance of the Stol Demonstration
750462	Weldbond and Its Performance in Aluminum Automotive Body Sheet
740388	A New Method of Bulkhead Analysis in Aircraft Structures
740258	A Review of Recent Developments in the Holographic Observation of Disbonds
740387	Shell Instability Analysis Using the Finite Element Method
740389	Structural Finite Element Analysis Aided By Computer Graphics
740386	The SnkDf Concept--A Method of Sn Data Development for Aluminum Aircraft Structures
730340	A Comparison of Structural Test Results With Predictions of Finite Element Analysis
730341	An Inexpensive, Full-Scale Aircraft Fatigue Test System
730348	B-1 Technology Applications to Advanced Transport Design
730339	Composites for Noise Control
730308	Stepped Aluminum Extrusions -- Designing for Business Aircraft
730338	Structural Cost Effectiveness of Composites
730307	Use of Honeycomb and Bonded Structures in Light Aircraft
720120	Adhesives for Naval Applications
720311	Fatigue Certification of General Aviation Aircraft in Australia
720305	Investigation of Flight Loads, Counting Methods, and Effects on Estimated Fatigue Life
710110	Adhesive Bonding of High Modulus Composite Aircraft Structures
700221	Bonded Aircraft Structures for General Aviation
700539	Design Considerations in Selecting Alloys for Aircraft Structures
700219	Fatigue Evaluation for Light Twin Engined Aircraft
700222	Loading Conditions Measured During Aerobatic Maneuvers
690342	Application of Glass-Reinforced Plastic Molding Compounds in the Ov-10a Airplane
680204	Design requirements of C-5A military cargo aircraft
680316	Application of Graphite Fiber Composites to Airframe Structures
680313	Designing and Fabricating Aircraft Structures With Filamentary Composites
680330	Use of Beryllium for Aircraft Structural Components
660216	Design and Development of the Structural Integrity of a Jet Executive Aircraft, D.H. 125
650388	A Practical Approach to Airplane Vibration
670257	Certification of the Sabreliner Twin Jet Executive Airplane, With Special Emphasis on Fatigue Evaluation of Structure
650055	Computerized Static and Dynamic Aircraft Structural Analysis System--Engineering Aspects and Mathematical Formulation of the Problem
650053	Computerized Static and Dynamic Aircraft Structural Analysis System--Historical Background
650056	Computerized Static and Dynamic Aircraft Structural Analysis System--Programming the System
650054	Computerized Static and Dynamic Aircraft Structural Analysis System--Use of Computer Programs in Aircraft Design
670259	Design of Pressurized Cabins for Business Aircraft
640308	Aircraft corrosion
640097	Bonded structures in the F-27
640034	Experience with reinforced plastic primary aircraft structures
630391	An application of brazed stainless steel honeycomb for moderately high temperature structures
630371	An investigation of structural concepts for a mach 3+ supersonic transport wing
630241	Designing structures for acoustic fatigue
620374	The B-70's new structural design concepts for mach 3 temperatures
610016	Mach 3 wing structures stiffened skin versus sandwich
610085	Reacting flight loads at forging temperatures
610379	Sonic proof testing B-58 weapons system
610250	Trends in light aircraft structural design
600045	Preliminary design considerations for the structure of a trisonic transport
580041	Designing with steel for lighter aircraft
580016	Problems in the application of high-strength steel alloys in the design of supersonic aircraft
580221	Use of adhesives in the aircraft industry
570194	Application of chem-mill to airframe structures
570156	The role of high strength weldments in aircraft structure
560002	Application of metallic materials for aircraft structures in the temperature range 600 to 1100 F
560039	Fatigue and fail-safe airframe design
560163	Forgings and modern fighter airplane producibility
560014	The selection of metals for airframe components as affected by operation at elevated temperatures up to 600 F
540155	A plan of attack on aircraft fatigue
540226	Design for fatigue
540151	Selection of aircraft construction materials
530149	The effect of temperature on aircraft structural design
530267	Titanium in airframes
530223	Today's aluminum aircraft alloys
520153	"Lockfoam" filled-in-place structures
520123	Chan-o-seal for modern aircraft
520115	Design of radomes resistant to gun blast
510129	Adhesion engineering
490206	Dynamic loads on airplane structures
480130	Structural aspects of high speed airplanes
480042	What price structural testing
470150	Comparison of use of mixed structural materials and fabric covering to all-metal construction for personal aircraft from a manufacturing viewpoint
470229	Experiences of an aircraft manufacturer with sandwich material
470094	Operational experience on the Lockheed Constellation~Powerplants, structure and accessories
470228	Philosophy for design of sandwich-type structure
460108	A summary of design and test experience with monocoque magnesium wings
460144	Simplified structures for low cost airplanes
460161	The development of magnesium alloys as aircraft materials
460022	Trends in aircraft structures
450124	Materials in bomber construction
450233	Wood versus metal construction in aircraft
440022	Design features of the mosquito aeroplane
430030	Aircraft structural testing
430047	Influence of new materials on the structural design of airplanes
430159	Problems in wood aircraft
420055	Structural materials for the cargo airplane
420045	Wood-plastics in mass production of aircraft
390019	A low-density material for aircraft structures
390162	Flush riveting considerations for quantity production
380017	Stainless steel for aircraft
370132	Problems in design and construction of large aircraft
360138	Manufacturing phases of metal-aircraft construction
360143	Stressed-skin structures for aircraft
350045	Aircraft structural design and its influence on other engineering design
320011	Late developments in airplane stress-analysis methods and their effect on airplane structures
310034	Weight saving by structural efficiency
300031	Weight saving by structural efficiency
290066	Prevention of corrosion in duralumin airplane structures
280030	Duralumin all-metal airplane construction
280027	Monoplane or biplane
270066	Metal construction of aircraft
270072	Modern Naval Aircraft
270065	Selection of materials for aircraft structures
260065	Economical production of all-metal airplanes and seaplanes
260026	Metalclad rigid airship development
250069	Some aspects of airplane inspection
170011	Evolution of airplane wing-trussing