This report is a compilation of the papers presented at the 1988 Structural Integrity Program Conference held at the Hilton Palacio del Rio Hotel, San Antonio, Texas on 29 November - 1 December 1988. Partial contents include: Propulsion & Power System Integrity; The Integrity Process as Applied to the F-119-PW-100 Advanced Tactical Fighter Engine; Structural Analysis, Fasteners & Testing ; Predicting Fatigue Crack Growth Under Combined Tension & Out of Plane Bending in Transitional Thickness Plates; Inspection of Fatigue Critical Fastener Holes Using Capacitance Measurement System Equipment; An update on the Study of the Quality of Screw Threaded Products; CF116 Full-Scale Durability and Damage Tolerance Test; F-16 Full-Scale AIrframe Durability Test; T37B Damage Tolerance Analysis Results; The C-17 Aircraft Structural Integrity Overview; The X-30 Structural Integrity Program; Structural Risk Analysis in Aging Aircraft Fleets; Metallic/Composite Structures; Low Velocity Impact Damage Detector Development. (KT)
Proceedings of the Structural Integrity Program Conference. Held in San Antonio, Texas on November 29-December 1, 1988
1989
958 pages
Report
No indication
English
Aircraft , Jet & Gas Turbine Engines , Structural Mechanics , Composite structures , Crack propagation , Aircraft engines , Fighter aircraft , Tactical aircraft , Fastenings , Engine components , Structural analysis , Structural properties , Symposia , Bending , Capacitance , Damage , Fatigue(Mechanics) , Holes(Openings) , Measuring instruments , Metals , Plates , Reliability , Risk , Test and evaluation , Thickness , Tolerance , Transitions , Metal Composites , F-119 Aircraft , PW-100 Engine