Investigation of Aerodynamic Forces on Scramjet Inlets Using Shock Tunnel Tests

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概要

• 論文の詳細を見る
• 1995-11-04

著者

• Yamazaki Takashi

  National Aerospace Laboratory

• ITO Takeshi

  National Aerospace Laboratory

関連論文

• An Experimental Study on the Boundary Layer Transition due to Gas Injection from Capsule-shape Body Surface
• Measurement of Hypersonic Flow Fields around a Sidewall Compression Scramjet Inlet Using Shock Tunnel Experiments
• Investigation of Aerodynamic Forces on Scramjet Inlets Using Shock Tunnel Tests

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