Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • General rotorcraft aeromechanical stability program (GRASP) theory manual [microform] / Dewey H. Hodges ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation Systems Command, Aviation Research and Technology Activity ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Flowfield of a lifting hovering rotor--a Navier-Stokes simulation [microform] / G.R. Srinivasan ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation Systems Command, Aviation Research and Technology Activity ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades [microform] / J.D. Baeder.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation Systems Command, Aviation Research and Technology Activity ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1991]
    • 1991

  • Design and evaluation of a cockpit display for hovering flight [microform] : final technical report / Ronald A. Hess and Peter James Gorder.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Performance optimization for rotors in hover and axial flight [microform] / T.R. Quackenbush ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Flow visualization studies of VTOL aircraft models during hover in ground effect [microform] / Nikos J. Mourtos ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A two dimensional study of rotor/airfoil interaction in hover [microform] / by Chyang S. Lee.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Palo Alto, Calif.] : Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • An experimental and analytical method for approximate determination of the tilt rotor research aircraft rotor-wing download [microform] : final report, 05-30-94 - 11-30-85 / principal investigator, David E. Jordan, William Patterson, Doral R. Sandia.

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University, Aeronautical Engineering Dept. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1985

  • An experimental and analytical investigation of isolated rotor flap-lag stability in forward flight [microform] : paper no. 66, September 10-13, 1985 / Gopal H. Caonkar, Michael J. McNulty, J. Nagabhushanam.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers [microform] / John C. Wilson and Henry L. Kelley.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, distributor], 1986.
    • 1986

  • Moving base simulation of an integrated flight and propulsion control system for an ejector-augmentor STOVL aircraft in hover [microform] / Walter E. McNeill ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Wide speed range turboshaft study [microform] / Martin D'Angelo.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Rotor vortex filaments [microform] : living on the slipstream's edge / Larry A. Young.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 199 ]
    • 1997

  • Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover [microform] / James A. Franklin and Michael W. Stortz.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Flow field around a hovering rotor [microform] / C. Tung and S. Low.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Aeroelastic stability of a full-scale hingeless rotor [microform] / Randall L. Peterson and Khanh Nguyen.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft [microform] / James A. Franklin.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Performance and pressure data from a small model tilt-rotor in hover [microform] / Lonnie Branum and Chee Tung.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • XV-15 structural-acoustic data [microform] / Karen H. Lyle.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover [microform] / John D. Lee and Rorry Harding and Richard L. Palko.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1984]
    • 1984

  • Simulation evaluation of a speed-guidance law for Harrier approach transitions [microform] / Vernon K. Merrick ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59835

  • The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover [microform] / William G. Bousman.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65436

  • Analysis of small-scale rotor hover performance data [microform] / Cahit Kitaplioglu.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67740

  • Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft [microform] / Russell V. Parrish, Steven P. Williams.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS66515

  • Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept [microform] / Donald R. Riley and Gautam H. Shah, Richard E Kuhn.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS72303

  • Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor [microform] / Arthur E. Phelps III and Susan L. Althoff.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986

  • Reconstruction of a three-dimensional transonic rotor flow field from holographic interferogram data [microform] / Yung H. Yu, John K. Kittleson, and Friedhelm Becker.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; St. Louis, Mo. : United States Army Aviation Systems Command, [1985]
    • 1985

  • Description of the U.S. Army small-scale 2-meter rotor test system [microform] / Arthur E. Phelps III and John D. Berry.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [St. Louis, MO] : U.S. Army Aviation Systems Command ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS93238

  • Results of the integration of a transonic full-potential analysis program with a free-wake lifting-line program for hovering rotors [microform] / Song-Young Chung.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92583

  • Navier-Stokes calculations for the vortex wake of a rotor in hover [microform] / C.H. Liu, J.L. Thomas, and C. Tung.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; St. Louis, Mo. : United States Army Aviation Systems Command, [1984]
    • 1984

  • Hover test of a full-scale hingeless helicopter rotor [microform] : aeroelastic stability, performance, and loads data / William Warmbrodt, Randall L. Peterson.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984

  • Effect of ground and/or ceiling planes on thrust of rotors in hover [microform] / Vernon J. Rossow.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104581

  • Experimental assessment of helicopter rotor turbulence ingestion noise in hover [electronic resource] / J.C. Simonich, R. H. Schlinker and R. K. Amiet.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113600

  • Experimental assessment of helicopter rotor turbulence ingestion noise in hover [microform] / J.C. Simonich, R. H. Schlinker and R. K. Amiet.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113600

  • Experimental study of main rotor tip geometry and tail rotor interactions in hover [microform] / D. T. Balch and J. Lombardi.

    • Text
    • Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • Analysis of a hovering rotor in icing conditions / Robert Narducci, Richard E. Kreeger.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo25020

  • Design study of propulsion and drive systems for the Large Civil TiltRotor (LCTR2) rotorcraft / Mark Robuck [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.
    • 2013-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53692

  • Aeromechanical stability of a hingeless rotor in hover and forward flight : analysis and wind tunnel tests / William T. Yeager, Jr., M-Nabil H. Hamouda, Wayne R. Mantay.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1983.
    • 1983-8

  • Rotating shake test and modal analysis of a model helicopter rotor blade / W. Keats Wilkie, Paul H. Mirick, and Chester W. Langston.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65480

  • A basic robotic excavator (the "Glenn digger٣) : description, design, and initial operation / Steve Bauman [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2016.
    • 2016-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68693

  • Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover / Anthony Neal Watkins [and five others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 2018.
    • 2018-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo111594

  • Aeromechanical stability of a hingeless rotor in hover and forward flight : analysis and wind tunnel tests / William T. Yeager, Jr., M-Nabil H. Hamouda, Wayne R. Mantay.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1983.
    • 1983-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62349

  • Hover test vehicle : implementation plan and test results.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, February 2009.
    • 2009-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo172780

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta