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Analysis of sonic boom measurements near shock wave extremities for flight near Mach 1.0 and for airplane accelerations /

Title:Analysis of sonic boom measurements near shock wave extremities for flight near Mach 1.0 and for airplane accelerations /
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Note:Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974
  
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Subject:Noise propagation
Subject:Acoustic properties
Subject:Acoustic measurement
Subject:Sonic booms
Subject:Pressure gradients
Subject:Overpressure
Subject:Atmospheric pressure
Subject:Aerodynamic noise
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