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- W2160544450 abstract "The Naval Air Warfare Center, Aircraft Division (NAWCAD) in cooperation with the Federal Aviation Administration (FAA) is sponsoring a Small Business Innovation Research (SBIR) Phase II program to investigate water impact dynamics relevant to DOD, DOT and industry. One of the primary objectives of the program is to develop analytical tools that can be used to facilitate the process of showing compliance with current civil and military ditching requirements with a decreasing dependence on expensive scale model ditching tests. This paper describes an effort that focuses on the application of a crash modeling and simulation approach utilizing both a nonlinear finite-element code (MSC/DYTRAN ® ) and a hybrid impact code (DRI/KRASH) to demonstrate the potential for airframe water impact analysis in the development of crash design criteria and concepts. The test recorded pressures, accelerations and damage from a fully instrumented UH-1H helicopter 26-ft/s vertical impact into water are presented. Pretest analyses using DRI/KRASH and MSC/DYTRAN" @default.
- W2160544450 created "2016-06-24" @default.
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- W2160544450 date "2000-05-02" @default.
- W2160544450 modified "2023-09-23" @default.
- W2160544450 title "Rotary Wing Aircraft Water Impact Test And Analyses Correlation" @default.
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- W2160544450 hasPublicationYear "2000" @default.
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