Accession Number:

ADA272876

Title:

Proceedings of the 1992 USAF Structural Integrity Program Conference Held in San Antonio, Texas on December 1 - 3, 1992.

Descriptive Note:

Final rept. 1-3 Dec 92,

Corporate Author:

WRIGHT LAB WRIGHT-PATTERSON AFB OH

Report Date:

1993-09-01

Pagination or Media Count:

894.0

Abstract:

Partial contents include the following 1 New developments in fatigue management of F-16 aircraft 2 Quantifying accuracy of fatigue life prediction methodology 3 Naval aircraft approach and landing data acquisition system 4 A diagnostic reasoning technology demonstrator for gas turbine engines 5 Cost effective risk management in design and flight qualification 6 a preliminary study of fatigue durability in terms of crack growth 7 A fatigue analysis of panels with multiple site damage 8 Probabilistic rotor design system 9 Assessment of helicopter component statistical reliability computations 10 The effects of negative R ratio on fatigue crack growth 11 Effect of microporosity on fatigue durability of thick 7050 aluminum plate 12 Fatigue and residual strength characteristics of fiber metal laminates subjected to incidental damage 13 The role of nondestructive inspection in an F-15E wing spar structural integrity program 14 Ultrasonic imaging system for F-4 lower torque box skin 15 Acoustic emission monitoring of the CF116 CF5 full-scale durability and damage tolerance test 16 Vibratory characterization of integrally bladed rotors utilizing surrogate blade models 17 F-4 lower wing skin integral stiffener failure analysis 18 New aircraft lower wing skin trade study 19 C-141 composite material repairs to metallic airframe components and 20 Repair of F-16 static discharge probes.

Subject Categories:

  • Aircraft
  • Jet and Gas Turbine Engines
  • Laminates and Composite Materials

Distribution Statement:

APPROVED FOR PUBLIC RELEASE