Wind Tunnel Studies Of The Pressure Distribution And The Flow Field In The Wake Of The Lockheed C-141A Starlifter Jet Transport Aircraft

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Report Number: AFFDL TR 67-163
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
Pages: 54
Contract: F33615-67-C-1010
DoD Project: 6065
DoD Task: 606503
Identifier: AD0835380

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Provenance: Lockheed Martin Missiles & Fire Control

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