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Numerical Analysis of the Transient Responce of Advanced Thermal Protection Systems for Atmosphereic Entry
Robert T. SwannClaud M. Pittman
其他書名
Robert T. Swann and Claud M. Pittman
出版National Aeronautics and Space Administration, 1962
URLhttp://books.google.com.hk/books?id=PCSzmJKCe28C&hl=&source=gbs_api
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註釋Equations for the transfer of heat through thermal protection shields are derived in finite difference form. These equations are applicable to charring ablators, impregnated ceramics, subliming ablators, heat sinks, and insulating materials and have been programmed for solution on a high speed digital computer.