The purpose of this conference was to bring together technical personnel in DOD and the aerospace industry involved in the various turbine engines, airframes and other mechanical systems. It provided a forum to exchange ideas relating to the critical aspects of durability and damage tolerance technology for aircraft systems. Session topics included: Structural analysis; Structural analysis and testing; Materials and nondestructive evaluation; ENSIP; and Force management.
Proceedings of the 1989 Structural Integrity Program Conference Held in San Antonio, Texas on 5-7 December 1989
1990
1033 pages
Report
No indication
English
Aircraft , Jet & Gas Turbine Engines , Jet engines , Jet aircraft , Airframes , Symposia , Structural components , Damage , Risk , Aircraft industry , Life expectancy(Service life) , Probability , Tolerances(Mechanics) , Structural analysis , Test methods , Nondestructive testing , Aging(Materials) , Aircraft equipment , Fatigue(Mechanics) , Cracks , Fatigue tests(Mechanics) , Repair , Finite element analysis , Jet transport aircraft , Jet bombers , Attack bombers , Jet training aircraft , Jet fighters , Jet engine nacelles , Wings , Spars , Aluminum alloys , Titanium alloys , Meetings , ENSIP(Engine Structural Integrity Program) , Damage tolerance , C-141 Aircraft , B-1 Aircraft , Smart structures , T-38 Aircraft , F-16 Aircraft , F-15 Aircraft , Durability , A-10 Aircraft , Tails(Aircraft) , Flight loads , Structural integrity , Composite materials , Inspection , Reliability