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Experimental studies of the unstedy aerodynamics of panels at or near flutter with a finite boundary layer Mach number 1 to 10

Title:Experimental studies of the unstedy aerodynamics of panels at or near flutter with a finite boundary layer Mach number 1 to 10
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Note:Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964
  
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Subject:Aerodynamic load
Subject:Flutter (Aerodynamics)
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