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  • High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test [microform] / Brent R. Cobleigh.

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

  • Design and numerical evaluation of full-authority flight control systems for conventional and thruster-augmented helicopters employed in NOE operations [microform] : interim report / Todd A. Perri, R.M. McKillip, Jr., H.C. Curtiss, Jr.

    • Text
    • Princeton, NJ : Princeton University, Dept. of Mechanical and Aerospace Engineering ; [Moffett Field, Calif. : NASA Ames Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Langley Symposium on Aerodynamics [microform] : proceedings of a symposium held at NASA Langley Research Center, Hampton, Virginia, April 23-25, 1985 / Sharon H. Stack, compiler.

    • Text
    • [Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1985.
    • 1985-present

  • Non-linear unsteady wing theory [microform] / J.E. McCune.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987-present

  • A survey of handling qualities criteria and their applications to high performance aircraft [microform] : final report / principal investigators, David L. Pearl, Faysal Kolkailah, 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

  • The performance evaluation of a jet flap on an advanced supersonic harrier [microform] : final report / principal investigators, Larry Dean Lipers, Doral R. Sandlin.

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University, Astronautical Engineering Dept. ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness [microform] / Eugene A. Morelli.

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

  • Dynamic forms. Part II, Application to aircraft guidance [microform] / George Meyer and G. Allan Smith.

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

  • F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack [microform] : contract NAS 3-26617 / Andrew J. Yuhas ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers [microform] / Patrick C. Stoliker and John T. Bosworth.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Cockpit displays to support hazard awareness in free flight [microform] : final technical report, ARL-97-7/NASA-97-4, contract NASA NAG 2-996 / C.D. Wickens ... [et al.].

    • Text
    • Savoy, Ill. : Aviation Research Laboratory, Institute of Aviation, University of Illinois at Urbana-Champaign ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Investigation of dynamic flight maneuvers with an iced tailplane [microform] / Judith Foss Van Zante, Thomas P. Ratvasky.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • High-alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle [microform] / Keith D. Wichman ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996

  • Investigation of piloting aids for manual control of hypersonic maneuvers [microform] / David L. Raney, Michael R. Phillips, and Lee H. Person, Jr.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54049

  • Rule-based air combat simulation [microform] / G. H. Burgin and L. B. Sidor.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58949

  • Full potential methods for analysis/design of complex aerospace configurations [microform] / Vijaya Shankar, Kuo-Yen Szema, and Ellwood Bonner.

    • Text
    • Los Angeles, Calif. : Rockwell International Corp. ; [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986

  • Candidate control design metrics for an agile fighter [microform] / Patrick C. Murphy, Melvin L. Bailey, Aaron J. Ostroff.

    • 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, 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60321

  • Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data [microform] / William T. Suit and James G. Batterson.

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

  • V/STOL maneuverability and control [microform] / James A. Franklin and Seth B. Anderson.

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

  • A flight investigation of roll-control sensitivity, damping, and cross-coupling in a low-altitude lateral maneuvering task [microform] / L. D. Corliss and G. Dean Carico.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; St. Louis, Mo. : United States Army Aviation Research and Development Command, [1983]
    • 1983

  • A flightpath overshoot flying qualities metric for the landing task [microform] / Donald T. Berry.

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

  • Aerodynamic parameters of an advanced fighter aircraft estimated from flight data : preliminary results / Vladislav Klein, Kevin P. Breneman, Thomas P. Ratvasky.

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS108722

  • Aerodynamic parameters of an advanced fighter aircraft estimated from flight data [microform] : preliminary results / Vladislav Klein, Kevin P. Breneman, Thomas P. Ratvasky.

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

  • The effect of faster engine response on the lateral directional control of a damaged aircraft / Ryan D. May ... [and others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo26324

  • Nonlinear aerodynamic modeling from flight data using advanced piloted maneuvers and fuzzy logic / Jay M. Brandon and Eugene A. Morelli.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo40345

  • Maneuver acoustic flight test of the Bell 430 helicopter data report / Michael E. Watts [and four others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2014.
    • 2014-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52363

  • Analysis and simulation of the simplified aircraft-based paired approach concept with the ALAS alerting algorithm in conjunction with echelon and offset strategies / Wilfredo Torres-Pomales [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2014.
    • 2014-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54368

  • High-Alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle / Keith D. Wichman [and six others]

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65674

  • F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack / Andrew J. Yuhas [and three others].

    • Text
    • Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66655

  • Pseudosteady-state analysis of nonlinear aircraft maneuvers / John W. Young, Albert A. Schy, and Katherine G. Johnson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71349

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