Accession Number : ADA213545


Title :   Proceedings of the Structural Integrity Program Conference. Held in San Antonio, Texas on 29 November-1 December 1988


Descriptive Note : Final technical rept. 29 Nov-1 Dec 1988


Corporate Author : WRIGHT RESEARCH AND DEVELOPMENT CENTER WRIGHT-PATTERSON AFB OH


Personal Author(s) : Cooper, Thomas D ; Lincoln, John W


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a213545.pdf


Report Date : May 1989


Pagination or Media Count : 958


Abstract : 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.


Descriptors :   *FIGHTER AIRCRAFT , *AIRCRAFT ENGINES , *ENGINE COMPONENTS , *COMPOSITE STRUCTURES , *CRACK PROPAGATION , *TACTICAL AIRCRAFT , *FASTENINGS , *STRUCTURAL ANALYSIS , *STRUCTURAL PROPERTIES , TEST AND EVALUATION , PLATES , CAPACITANCE , TRANSITIONS , FATIGUE(MECHANICS) , TOLERANCE , MEASURING INSTRUMENTS , HOLES(OPENINGS) , RELIABILITY , BENDING , METALS , THICKNESS , SYMPOSIA , RISK , DAMAGE


Subject Categories : Aircraft
      Laminates and Composite Materials
      Metallurgy and Metallography
      Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE