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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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