SAE Papers

Paper Number	Paper Title	Book Number
2-28-5-40	Aerospace proves its metal
2-28-1-26	Casting a vote for alloys
2-25-8-16	Advanced Materials for Manufacturability
2-23-9-21	Laser-Welding Aluminum
1999-01-2284	Blind Fastener Inflation for Structural Joining of Aluminum
1999-01-1564	Hole Quality Study in High Speed Drilling of Composite and Aluminum Sheet Metal
1999-01-1574	Residual Strength of An Aluminum Panel With a Centric Hole and One Cracked Ligament
983118	Dual Torch Plasma De-Painting of Aluminum Substrates
941844	Aluminum-Lithium (Alloy 2090) Fastening Evaluation for Commercial Aircraft Applications
931229	Environmental Durability of Aircraft Aluminum Alloy Skin Materials
900959	The Use of Improved Corrosion Resistant Aluminum Alloy 6013 on the NavyS P-7a Aircraft
890925	Manufacturing and Handling Techniques Used in the Assembly of Polished Commercial Aircraft
881404	Aluminium-Lithium Alloy Forgings for Aerospace
881405	Fracture Mechanics Characteristics of Laser-Welded Aluminum-Lithium Sheet Joints
881551	Turbine Technology-Materials Set the Pace
880874	How to Make the Successful Transition From a Painted to a Polished Aluminum Aircraft Fleet
870748	The Economic Advantages of Operating a Polished Aluminum Aircraft Fleet
861627	Alternate Launch and Recovery Surface Traction Characteristics
861836	Leakage Characteristics of Gas Screw Seals
861850	The Cost Effectiveness of Weight Reduction By Advanced Material Substitution
841514	A Novel Approach for Rapid Solidification Processing of High Strength Pm Aluminum Alloys
831441	Elevated Temperature Aluminum Alloys for Aerospace Applications
730891	Application of Advances in Structures and Materials to the Design of the Yf-17 Airplane
730884	Material Selection Procedures for Advanced Transport Aircraft
710801	Control of Warpage During Machining
690689	Comparison of a Typical Eutectic Superalloy Containing Nickel, Aluminum, and Columbium (Niobium) With Commercially Available Superalloys
680648	Systems Considerations for Aerospace Beryllium Applications
670861	Metal-Matrix Composites Show Promise for Aerospace Applications
660665	Aluminum, Titanium, Beryllium, Iron, and Nickel Alloys for Structures of High-Altitude High-Temperature Vehicles
660652	Comparison of Lightweight Structural Materials--Beryllium and Its Alloys With Magnesium, Aluminum, and Titanium
660677	Design of Storable Propellant Pressure Vessels
660292	Developments in Aluminum Welding
660678	Hypersonic Aircraft Thermal-Structural Concept Trends
660679	Structural Considerations in the Design of a Liquid Hydrogen Tank for Hypersonic Vehicles
650785	Cost/Weight Merit Function for Aerospace Hardware Design
650754	Joining Aluminum to Stainless Steel for Space Vehicle Applications
650779	Press Bonding of Apollo Cold Plates
650790	Problems of Transition From Aluminum to Exotic Materials in Aerospace Structures
630407	Survey of candidate aluminum materials for supersonic aircraft applications
380119	Quality control of aluminum-alloy aircraft castings
360083	Designing for the use of aluminum alloy forgings and extrusions in aircraft production