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Effect of jet velocity and axial location of nozzle exit on the performance of a twin-jet afterbody model at Mach numbers up to 2.2 /

Title:Effect of jet velocity and axial location of nozzle exit on the performance of a twin-jet afterbody model at Mach numbers up to 2.2 /
Author:
Author:
Author:
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Note:Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1969
  
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Subject:Drag (Aerodynamics)
Subject:Supersonic nozzles
Subject:Supersonic wind tunnels
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