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Design, Fabrication, Testing, And Data Analysis Of Adam II Concept (Propulsive Wing). Part IV. Testing In The Langley Research Center 16-Foot Transonic Wind Tunnel
Author(s): English, Robert B., Davidson, Jim K., Brownrigg, William E., Jr.
Corporate Author(s): LTV Aerospace Corp Dallas Tx Vought Aeronautics Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 68-31 Part 4

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