The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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

Report Number: AFFDL TR 67-163
Author: Goodrick, T. F.
Corporate Author: 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
Project: 6065
Task: 606503
AD Number: AD0835380

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Lockheed Martin Missiles & Fire Control
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