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![AFFDLTR68-031part01.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/a1f760b608c1efeff6614d17b8e7b98e0141a222.jpg)
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Design, Fabrication, Testing, And Data Analysis Of Adam II Concept (Propulsive Wing). Part I, General And Summary Information
Author(s): McClure, James G., Shumway, Justin F., Cragin, Glen P., JrCorporate 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 1
![AFFDLTR68-031part02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/d5f26e48f2f99cc72e002777e13eef817def700a.jpg)
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Design, Fabrication, Testing, And Data Analysis Of Adam II Concept (Propulsive Wing). Part II. Shakedown Testing In Vad 7-Ft X 10-Ft Low Speed Wind Tunnel
Author(s): Meyer, Robert D., English, Robert B., Davidson, Jim K.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 2
![AFFDLTR68-031part03.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/98ea67483b28098873294cfe736d4824f4f1d8ef.jpg)
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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
![AFFDLTR68-031part04.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/4f53a5089301f5e88137b1db7d86f2362710ea1c.jpg)
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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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