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  • Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control [microform] / Scott C. Asbury and Craig A. Hunter.

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

  • The control system for the X-33 linear aerospike engine [microform] / Jerry E. Jackson, Erich Espenschied, Jeffrey Klop.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Optimal pitch thrust-vector angle and benefits for all flight regimes [microform] / Glenn B. Gilyard, Alexander Bolonkin.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 2000]
    • 2000

  • Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept [microform] / David J. Wing.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • STOVL Control Integration Program [microform] / C. Weiss, P. McDowell and S. Watts.

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

  • High-Alpha Research Vehicle (HARV) longitudinal controller : design, analyses, and simulation results [microform] / Aaron J. Ostroff, Keith D. Hoffler, Melissa S. Proffitt.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.

    • 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

  • Xenon ion propulsion for orbit transfer [microform] / V.K. Rawlin, M.J. Patterson, and R.P. Gruber.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Design and evaluation of thrust vectored nozzles using a multicomponent thrust stand [microform] : final progress report, 10-01-88 - 01-31-90 / Thomas W. Carpenter, principal investigator ... [et al.].

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Fourth High Alpha Conference, NASA Dryden Flight Research Center, Edwards, California, July 12-14, 1994 [microform]

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

  • Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Design of power electronics for TVC & EMA systems [microform] ; final report / R. Mark Nelms, J. Brett Bell, and Michael T. Shepherd.

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

  • Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels [microform] / Milton Lamb.

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

  • Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows [microform] / by Scott T. Imlay.

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

  • An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques [microform] : final report / by William G. Schweikhard and Werachone N. Singnoi.

    • Text
    • Lawrence, Kan. : University of Kansas ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1995

  • 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

  • Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0̊ to 70̊ [microform] / Scott C. Asbury and Francis J. Capone.

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

  • Design specification for a thrust-vectoring, actuated-nose-strake flight control law for the high-alpha research vehicle [microform] / Barton J. Bacon ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle [microform] / W. Thomas Bundick ... [et al].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • HARV ANSER flight test data retrieval and processing procedures [microform] / Jessie C. Yeager.

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

  • An experimental/modeling study of jet attachment during counterflow thrust vectoring [microform] : final report, NASA/NAG1-1736, grant period 1 July, 1995 - 30 June, 1996 / principal investigator, Paul J. Strykowski.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Integrated control using the SOFFT control structure [microform] : under contract NAS1-20185 / Nesim Halyo.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability [microform] / David J. Wing, Charles T.L. Mills, and Mary L. Mason.

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

  • Development and flight test of an augmented thrust-only flight control system on an MD-11 transport airplane [microform] / Frank W. Burcham, Jr. ... [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

  • An overview of the NASA F-18 High Alpha Research Vehicle [microform] / Albion H. Bowers ... [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

  • Design and integration of an actuated nose strake control system [microform] / Bradley C. Flick ... [et al.].

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

  • Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application [microform] / Jack (Jagdish) S. Sokhey and Baily R. Vittal, David W. Lam.

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

  • Electro-mechanical actuator [microform] : DC resonant link controller / Kenneth E. Schreiner.

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

  • Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing.

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

  • Flight testing the X-36--the test pilot's perspective [microform] / Laurence A. Walker.

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

  • A control law design method facilitating control power, robustness, agility, and flying qualities tradeoffs, CRAFT [microform] / Patrick C. Murphy and John B. Davidson.

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

  • High-alpha research vehicle lateral-directional control law description, analyses, and simulation results [microform] / John B. Davidson ... [et al.].

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

  • Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft [microform] / Martin J. Brenner.

    • 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

  • Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang.

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

  • A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane [microform] / Frederick J. Lallman, John B. Davidson, and Patrick C. Murphy.

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

  • Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes [microform] / Robert J. Foley, Odis C. Pendergraft, Jr.

    • 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

  • Relative control effectiveness technique with application to airplane control coordination [microform] / Frederick J. Lallman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service,] 1985.
    • 1985

  • Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles [microform] / Mary L. Mason and Bobby L. Berrier.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
    • 1985

  • Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability [microform] / Mary L. Mason and James R. Burley II.

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

  • Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap [microform] / Richard J. Re and Laurence D. Leavitt.

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

  • Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability [microform] / Linda S. Bangert and Laurence D. Leavitt.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60139

  • Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel [microform] / Albert L. Johns, ... [et al.].

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62061

  • Electromechanical actuation for thrust vector control applications [microform] / Mary Ellen Roth ; prepared for the National Aerospace and Electronics Conference (NAECON) sponsored by the Institute of Electrical and Electronics Engineers, Dayton, Ohio, May 21-25, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS66770

  • Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring" [microform] : June 11, 1989-December 10, 1989 / by J.B. Tseng and C. Edward Lan.

    • Text
    • Lawrence, Kan. : Flight Research Laboratory, University of Kansas Center for Research ; [Washington, D.C. : National Aeronautics and Space Administration, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69319

  • Propulsion and control propellers with thruster nozzles primarily for aircraft applications [microform] / W. Pabst.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986

  • Solid rocket booster thrust vector control subsystem description [microform] / compiled by John Redmon, Jr.

    • Text
    • [ Huntsville, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS98999

  • Noise generated by a flight weight, air flow control valve in a vertical takeoff and landing aircraft thrust vectoring system [microform] / Ronald G. Huff.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS105621

  • Pressure measurements of impinging jet with asymmetric nozzle : progress report / principal investigator: Ho, Chih-Ming.

    • Text
    • Los Angeles, Calif. : Dept. of Aerospace Engineering, University of Southern California ; Hampton, VA : NASA Langley Research Center, [1988]
    • 1988
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112097

  • Pressure measurements of impinging jet with asymmetric nozzle [microform] : progress report / principal investigator: Ho, Chih-Ming.

    • Text
    • Los Angeles, Calif. : Dept. of Aerospace Engineering, University of Southern California ; Hampton, VA : NASA Langley Research Center, [1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112097

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