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NASA TN D-1781

Title:NASA TN D-1781
Alternate title:Effects of nose bluntness, fineness ratio, cone angle, and model base on the static aerodynamic characteristics of blunt bodies at Mach numbers of 1.57, 1.80, and 2.16 and angles of attack up to 180 ̊
Note:National Aeronautics and Space Administration ;, 1963
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Subject:Angle of attack (Aerodynamics)
Subject:Blunt bodies -- Aerodynamics
Subject:Cone -- Aerodynamics
Subject:Noses (Space vehicles) -- Aerodynamics
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