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Rapid Shelter Flooring And Helicopter Landing Sites
Author(s): Gifford, F., Bilelo, A. M., Pascador, G., Rembert, R. S.
Corporate Author(s): LTV Aerospace Corp Dallas Tx Vought Aeronautics Div
Date of Publication: 1967-05
Report number: AFAPL TR 67-43
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Rapid Site Preparation Techniques. Prevention of Soil Erosion on an Earth-Filled Aircraft Shelter
Author(s): Doughty, Leon E., Jr
Corporate Author(s): LTV Aerospace Corp Dallas Tx Vought Aeronautics Div
Date of Publication: 1968-06
Report number: AFAPL TR 68-108
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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., 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 1
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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
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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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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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