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Design, Fabrication, Testing, And Data Analysis Of Adam II Concept (Propulsive Wing). Part III, Testing In 17 Ft Test Section Of 7 Ft X 10 Ft Wind Tunnel, Nasa Langley Research Center
Author(s): Brownrigg, William E., Jr., English, Robert B., Meyer, Robert D.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 3
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