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Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 /

Title:Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 /
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Note:Washington, D.C. : National Aeronautics and Space Administration, 1959
  
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Subject:Noses (Aircraft)
Subject:Shells (Engineering)
Subject:Wind tunnel testing
Subject:Hypersonic planes
Subject:Mach number
Subject:Aerodynamic measurements
Subject:Aerodynamics
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