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Critical sting length as determined by the measurement of pitch-damping derivatives for laminar, transitional, and turbulent boundary layers at Mach number 3 for reduced frequencies of 0.0033 and 0.0056

Title:Critical sting length as determined by the measurement of pitch-damping derivatives for laminar, transitional, and turbulent boundary layers at Mach number 3 for reduced frequencies of 0.0033 and 0.0056
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Note:Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynaqmics Facility, Air Force Systems Command, United States Air Force, 1977., 1977
  
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Subject:Pitching (Aerodynamics)
Subject:Supersonic wind tunnels
Subject:Turbulent boundary layer
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