Research Catalog

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  • Forward sweep, low noise rotor blade [microform] / inventor, Thomas F. Brooks.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Lateral stability analysis for X-29A drop model using system identification methodology [microform] / David L. Raney and James G. Batterson.

    • Text
    • [Washington, DC] : 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

  • The aluminum falcon [microform] : a low cost modern commercial transport / Non-Solo Design Group.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Preliminary flight assessment of the X-29A advanced technology demonstrator [microform] / John W. Hicks and Neil W. Matheny.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; Springfield, VA : National Technical Information Service], 1987.
    • 1987

  • In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft) [microform] / Edwin J. Saltzman, John W. Hicks.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • A correlation study of X-29A aircraft and associated analytical development [microform] / by Ali Ahmadi, Kajal Gupta, Paul Fortin.

    • Text
    • Lawrence, Kan. : University of Kansas Center for Research ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • The use of a panel code on high lift configurations of a swept forward wing [microform] : final report / principal investigators, James Scott Scheib, Doral R. Sandlin.

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

  • Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft [microform] / Gerald D. Budd.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service, 1984]
    • 1984

  • Body-freedom flutter of a 1/2 scale forward-swept-wing-model, an experimental and analytical study [microform] / Richard Chipman, ... [et al.].

    • Text
    • Bethpage, N.Y. : Grumman Aerospace Corporation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88328

  • X-29 flight-research program [microform] / Terrill W. Putnam.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • Dynamics and controls flight testing of the X-29A airplane [microform] / Joseph Gera.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
    • 1986

  • Dynamics and control of forward swept wing aircraft / principal investigators : Dr. David K. Schmidt, Dr. Terrence A. Weisshaar.

    • Text
    • West Lafayette. IN : School of Aeronautics and Astronautics, Purdue University ; Hampton. VA : NASA Langley Research Center, February 10. 1984.
    • 1984-210
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52155

  • Dynamics and control of forward swept wing aircraft / principal investigators: Dr. David K. Schmidt, Dr. Terrence A. Weisshaar.

    • Text
    • West Lafayette. Indiana : School of Aeronautics and Astronautics, Purdue University ; Hampton. Virginia : NASA Langley Research Center, February 10. 1984.
    • 1984-210

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