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29 items

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Design Studies and Model Tests of the Stowed Tilt Rotor Concept: Volume III - Appendixes
Author(s): Fry, Bernard L.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-07
Report number: AFFDL TR 71-62 Volume 3
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Volume IV. Wind Tunnel Test of the Conversion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model: Part I. Analysis and Results
Author(s): Magee, John, Taylor, Robert
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-08
Report number: AFFDL TR 71-62 Volume 4 Part 1
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Volume V. Wind Tunnel Test of a Powered Tilt-Rotor Perfromance Model
Author(s): Magee, John P., McHugh, Frank J., Miller, Nelson, DeLarm, Leon N., Taylor, Robert B.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-10
Report number: AFFDL TR 71-62 Volume 5
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Volume VI. Wind Tunnel Test of a Powered Tilt-Rotor Dynamic Model on a Simulated Free Flight Suspension System
Author(s): Tomassoni, John E., Delarm, Leon N., Schagrin, Edward B., Taylor, Robert B.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-10
Report number: AFFDL TR 71-62 Volume 6
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Volume VII. Wind Tunnel est of the Aerodynamics and Dynamics of Rotor Spinup, Stopping and Folding on a Semispan Folding Tilt-Rotor Model
Author(s): van Wagensveld, Dirk, Delarm, Leon N., Lapinski, Walter L., Magee, John P., McHugh, Frank J.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-10
Report number: AFFDL TR 71-62 Volume 7
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Design Studies and Model Tests of the Stowed Tilt Rotor Concept: Volume IX. Value Engineering Report
Author(s): Liiva, Jaan, Rose, H. J.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-10
Report number: AFFDL TR 71-62 Volume 9
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Volume IV. Wind Tunnel Test of the Concersion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model: Part II. Blade Stress Analysis, Bench Tests, and Wind Tunnel Model Details
Author(s): Magee, John, Taylor, Robert
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-08
Report number: AFFDL TR 71-62 Volume 4 Part 2
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V/STOL Dynamics and Aeroelastic Rotor-Airframe Technology
Author(s): Alexander, H. R., Leone, P. F.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-01
Report number: AFFDL TR 72-40 Volume 1
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STOL Tactical Aircraft Investigation Volume VI Air Cushion Landing System Study
Author(s): Gardner, Lloyd H., Milns, Peter, Pizzichemi, Charles J.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-05
Report number: AFFDL TR 73-19 Volume 6
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STOL Tactical Aircraft Investigation Volume V, Part I Flight Control Technology: System Analysis and Trade Studies for a Medium STOL Transport with Vectored Thrust/Mechanical Flaps
Author(s): Crandall, Kenneth J., Maund, David J., Gerken, William E., Vincent, James H.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-05
Report number: AFFDL TR 73-19 Volume 5 Part 1

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