Proceedings of the 1992 USAF Structural Integrity Program Conference Held in San Antonio, Texas on December 1 - 3, 1992
Proceedings of the 1992 USAF Structural Integrity Program Conference Held in San Antonio, Texas on December 1 - 3, 1992
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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 information
Proceedings of the 1992 USAF Structural Integrity Program Conference Held in San Antonio, Texas on December 1 - 3, 1992
1993
896 pages
Report
No indication
English
Aircraft , Jet & Gas Turbine Engines , Composite Materials , Engineering Materials , Gas turbines , Helicopters , Aircraft engines , Structural analysis , Composite materials , Structural response , Wings , Fatigue(Mechanics) , Rotor blades , Failure(Mechanics) , Cost effectiveness , Laminates , Crack propagation , Risk , Fatigue life , Static dischargers , Tolerances(Mechanics) , Nondestructive testing , Ultrasonic tests , Stiffening , Airframes , Skin(Structural) , Aging(Materials) , Strength(Mechanics) , Buffeting , Neural nets , Vibration , Aluminum , Repair , Damage assessment , Aircraft landings , Data acquisition , Structural integrity , Meetings , F-16 Aircraft , Stiffeners