Airframes -- Fatigue

Fatigue and fail-safe evaluation of flight structure and pressurized cabin for part 23 airplanes.

United States Federal Aviation Administration

Residual strength tests on Dove centre section tension booms

by R. Ellis and D. G. Graff.

Failure mechanisms of laminates transversely loaded by bolt push-through

William Allen Waters, Jr. and Jerry G. Williams.

Opening of an interface flaw in a layered elastic half-plane under compressive loading

John M. Kennedy, W.B. Fichter and James G. Goree.

Failure behavior of generic metallic and composite aircraft structural components under crash loads

Huey D. Carden and Martha P. Robinson.

Fracture mechanics design methodology.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Structures and Materials Panel.

The United Kingdom contribution to the AGARD 'fatigue-rated fastener systems' programme

by R. Cook.

Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement

William P. Henderson and William K. Abeyounis

In-flight breakup over the Atlantic Ocean, Trans World Airlines Flight 800 Boeing 747-131, N93119, near East Moriches, New York, July 17, 1996

National Transportation Safety Board.

Assuring the safety of the aging airline fleet: hearings before the Subcommittee on Aviation of the Committee on Public Works and Transportation, House of Representatives, One Hundred First Congress, first session, September 27, 1989; October 10, 1989

United States. Congress. House. Committee on Public Works and Transportation. Subcommittee on Aviation