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原文传递 Aircraft Crash Survival Design Guide. Volume III. Aircraft Structural Crashworthiness

题名：	Aircraft Crash Survival Design Guide. Volume III. Aircraft Structural Crashworthiness
作者：	Turnbow, J. W.;Tanner, A. E.;Singley III, G. T.;Laananen, D. H.;
关键词：	AVIATION ACCIDENTS, ARMY AIRCRAFT, CRASH RESISTANCE, COMPUTERIZED SIMULATION, IMPACT, COCKPITS, LOADS(FORCES), DYNAMIC RESPONSE, HELICOPTER ROTORS, STRENGTH(MECHANICS), SURVIVAL(GENERAL), HELICOPTERS, FUSELAGES, CARGO, AIRFRAMES, SURVIVAL(PERSONNEL), AVIATION SAFETY, FIXED WING AIRCRAFT, STRUCTURAL COMPONENTS, LANDING GEAR, CRASHES, DIRECTIONAL.
摘要：	This five-volume document has been assembled to assist design engineers in understanding the problems associated with the development of crashworthy U. S. Army aircraft. It includes not only a collection of available information and data pertinent to aircraft crashworthiness but suggested design conditions and criteria as well. Volume III contains information on the design of aircraft structures and structural elements for improved crash survivability. Current requirements for structural design of U. S. Army aircraft pertaining to crashworthiness are discussed. Principles for crashworthy design are presented in detail for the landing gear and fuselage subject to a range of crash conditions, including impacts that are primarily longitudinal, vertical, or lateral in nature and those that involve more complicated dynamic conditions, such as rollover. Analytical methods for evaluating structural crashworthiness are described.
总页数：	272
报告类型：	科技报告