Proceedings of the 1992 USAF Structural Integrity Program Conference Held in San Antonio, Texas on December 1 - 3, 1992.
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1993
- Accession Number
- ADA272876
Entities
People
- John W. Lincoln
- Robert M. Bader
- Thomas D. Cooper
Organizations
- Wright Laboratory