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Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium

Title:Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium
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Note:National Aeronautics and Space Administration ;, 1977
  
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Subject:Aerodynamics, Hypersonic -- Mathematical models
Subject:Fluid mechanics -- Mathematical models
Subject:Gas flow -- Mathematical models
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