The purpose of this 1993 Conference was to bring together technical personnel in DoD and the aerospace industry who are involved in the various technologies required to ensure the structural integrity of aircraft gas turbine engines, airframes and other mechanical systems. It provided a forum to exchange ideas and share new information relating to the critical aspects of durability and damage tolerance technology for aircraft systems.
Proceedings of the USAF Structural Integrity Program Conference Held in San Antonio, Texas on November 30-December 2, 1993
1994
864 pages
Report
No indication
English
Aircraft , Composite Materials , Nonferrous Metals & Alloys , Materials Degradation & Fouling , Structural Mechanics , Composite materials , Aluminum alloys , Structural analysis , Aging(Materials) , Aircraft engines , Epoxy composites , Transport aircraft , Mechanical properties , Aerospace industry , Fighter aircraft , Aviation accidents , Polymers , Matrix materials , Structural response , Flight testing , Altitude , Test and evaluation , Stress analysis , Airframes , Wings , Fuselages , Tolerances(Mechanics) , Damage assessment , Pitting , Failure(Mechanics) , Corrosion , Jet aircraft , Strength(Mechanics) , Cost effectiveness , Naval aircraft , Aircraft landings , Fatigue(Mechanics) , Crack propagation , Load distribution , Structural integrity , Aircraft structures , Meetings , Smart structures , F-15A Aircraft , F-15C Aircraft , C-17A Aircraft , C-141B Aircraft , T-38 Aircraft , F-15C/D Aircraft , B-1B Aircraft