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![AFFDLTR67-163.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/996b9f8d00c33fa3abdaefadb52902bcbab5a18b.jpg)
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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
![AFFDLTR68-015.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/7b6a3d3d50e374003d8d95a74494ecf9175aa1ac.jpg)
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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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