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Wind Tunnel Studies Of The Pressure Distribution And The Flow Field In The Wake Of The Lockheed C-141A Starlifter Jet Transport Aircraft
Author(s): Goodrick, T. F.Corporate Author(s): Minnesota Univ Minneapolis Dept Of Aeronautics And Engineering Mechanics
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 67-163
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Behavior of Extraction Parachutes in the Wake of a Powered Airplane Model.
Author(s): Heinrich, Helmut G., Hulcher, G. D.Corporate Author(s): Minnesota Univ Minneapolis Dept Of Aeronautics And Engineering Mechanics
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-08
Report number: AFFDL TR 68-15
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