A Self-consistent Tension Shell Structure for Application to Aerobraking Vehicle and its Aerodynamic Characteristics
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概要
- 論文の詳細を見る
A new method determining a tension shell structure for an application to an aerobraking vehicle is proposed. In this method, the tension shell configuration can be determined self-consistently in that the pressure distribution which is used to determine the shell configuration can be consistent with the one appearing on the configuration. The aerodynamic characteristics of the tension shell is also investigated numerically.
- 宇宙航空研究開発機構の論文
著者
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ABE Takashi
The Institute of Space and Astronautical Science
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Abe T
Inst. Space And Astronautical Science Kanagawa
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Abe Takashi
The Institute Of Physical And Chemical Research
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