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Development of Computational Models for Simulating Full-Scale Crash Tests of Aircraft Fuselage and Components.
| 题名： | Development of Computational Models for Simulating Full-Scale Crash Tests of Aircraft Fuselage and Components. |
| 关键词： | components；development；scale；models；fuse；ests；ompu；full；section；craft |
| 摘要： | In November 2000, a vertical drop test of a Boeing 737 airplane fuselage section was conducted at the Federal Aviation Administration (FAA) William J. Hughes Technical Center, Atlantic City International Airport, New Jersey. The intent was to determine the impact response of a narrow-body airplane fuselage section, including the response of the airframe structure and cabin items of mass. The purpose of this study was to develop a finite element model to simulate the vertical drop test of that fuselage section. The 10-foot-long test section included 18 seats occupied by dummy passengers, luggage stowed in the cargo compartment beneath the floor, and two different FAA-certified overhead stowage bins. The test article was dropped from a 14-foot height, resulting in a vertical impact velocity of 30 ft/sec. The primary goal of this drop test was to characterize the behavior of the two overhead bins under a severe, but survivable, impact condition. |
| 报告类型： | 科技报告 |
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