Research Catalog

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

Selected filters.Clear Filters

  • Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model [microform] / Stacey J. Cotton and Lisa J. Bjarke.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A preliminary look at techniques used to obtain airdata from flight at high angles of attack [microform] / Timothy R. Moes and Stephen A. Whitmore.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Wing pressure distributions from subsonic tests of a high-wing transport model [microform] / Zachary T. Applin and Carl L. Gentry, Jr., M.A. Takallu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Wake shape and its effects on aerodynamic characteristics [microform] / Homayoun Emdad and C. Edward Lan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept [microform] / A.M. Springer.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Evaluation of F/A-18A HARV inlet flow analysis with flight data [microform] / C. Frederic Smith ... [et al.].

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

  • Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing [microform] / Brenda E. Gile Laflin ... [et al.].

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

  • Euler technology assessment for preliminary aircraft design [microform] : unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration / Todd R. Michal.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : Available from the National Technical Information Service, [1998]
    • 1998

  • Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70̊ / Holly M. Ross, Scott P. Fears, and Thomas M. Moul.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60753

  • Determination of corrections to flow direction sensor measurements over an angle-of-attack range from 0⁰ to 85⁰ [microform] / Thomas M. Moul.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96293

  • Evaluation of a flow direction probe and a pilot-static probe on the F-14 airplane at high angles of attack and sideslip [microform] / Terry J. Larson.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS100007

  • STEP and STEPSPL--computer programs for aerodynamic model structure determination and parameter estimation / James G. Batterson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS105306

  • STEP and STEPSPL--computer programs for aerodynamic model structure determination and parameter estimation [microform] / James G. Batterson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS105306

  • Methods for estimating stability and control derivatives of conventional subsonic airplanes.

    • Text
    • [Lawrence? Kan.], [1971]
    • 1971
    • 1 Item
    FormatCall NumberItem Location
    Text TL574.S7R57Off-site

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