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SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
2008-01-2232
Operational Loads Monitoring of a Fleet of Beech 1900D Aircraft
 
2008-01-2266
Outsourcing Aircraft Maintenance Designed Around Safety, Diversification, and Performance
 
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 Aeroelastic 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
 
985601
Wing Manufacturing: Next Generation
 
981732
Radiator Wing Rotation Algorithm Overview for the International Space Station's External Active Thermal Control System
 
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
 
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 - Aerometr® 100 Alloy
 
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 Helicopter's 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 for 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!
 
872325
Correlation of Entrainment and Lift Enhancement for a Two-Dimensional Propulsive Wing
 
872458
A Frequency Domain Mimo Modal Identification Method with Application in the Aircraft Ground Vibration Test
 
872419
Mission-Adaptive Wing
 
871022
Certification of Bonded Composite Structure
 
860811
Three-Dimensional Traveling Load Finite Element
 
850893
Design and Use of KEVLAR® 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 SNKf 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
 
720305
An Investigation of Flight Loads, Counting Methods, and Effects on Estimated Fatigue Life
 
720311
Fatigue Certification of General Aviation Aircraft in Australia
 
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
Unique Design Considerations for a Large “T” Tail Aircraft
 
680330
Advancements in Structural Beryllium Technology
 
680313
Designing and Fabricating Aircraft Structures with Filamentary Composites
 
680316
The Application of Graphite Fiber Composites to Airframe Structures
 
670257
Certification of the Sabreliner Safe-Life Structure
 
670259
The Design of a Small Pressurized Aircraft Structure
 
660216
Design and Development of the Structural Integrity of a Jet Executive, D.H. 125
 
650388
Airplane Vibration - A Practical Approach
 
650055
Engineering Aspects and Mathematical Formulation of the Problem of a Computerized Aircraft Structural Analysis System
 
650053
Historical Background
 
650056
Programming the System
 
650054
Use of Computer Programs in Aircraft Design
 
640308
Aircraft Corrosion
 
640034
Experience with Reinforced Plastic Primary Aircraft Structures
 
630371
AN INVESTIGATION OF STRUCTURAL CONCEPTS FOR A MACH 3+ SUPERSONIC TRANSPORT WING
 
630391
An Application of Brazed Stainless Steel Honeycomb for Moderately High Temperature Structures
 
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
 
560163
FORGINGS AND MODERN FIGHTER AIRPLANE PRODUCIBILITY
 
560039
Fatigue and Fail-Safe Airframe Design
 
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
 
520123
CHAN-O-SEAL FOR MODERN AIRCRAFT
 
520115
DESIGN OF RADOMES RESISTANT TO GUN BLAST
 
520153
“LOCKFOAM” FILLED-IN-PLACE STRUCTURES
 
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 - (Powerplant, 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 vs METAL CONSTRUCTION IN AIRCRAFT
 
440022
DESIGN FEATURES OF THE MOSQUITO AEROPLANE
 
430030
AIRCRAFT STRUCTURAL TESTING
 
430047
INFLUENCE OF NEW MATERIALS ON THE STRUCTURAL DESIGN 0F 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, 1931
 
300031
Weight Saving by Structural Efficiency, 1930
 
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 ALLMETAL AIRPLANES AND SEAPLANES
 
260026
METALCLAD RIGID AIRSHIP DEVELOPMENT1
 
250069
SOME ASPECTS OF AIRPLANE INSPECTION
 
170011
EVOLUTION OF AIRPLANE WING-TRUSSING
 

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