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  • Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Design of supersonic transport flap systems for thrust recovery at subsonic speeds [microform] / Michael J. Mann, Harry W. Carlson and Christopher S. Domack.

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

  • Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study [microform] / C. Frederic Smith and Steve D. Podleski.

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

  • Effect of passive venting on static pressure distributions in cavities at subsonic and transonic speeds [microform] / Robert L. Stallings, Jr. ... [et al.].

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

  • The development of a highly reliable power management and distribution system for civil transport aircraft [microform] / Anthony S. Coleman and Irving G. Hansen.

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

  • On the use of controls for subsonic transport performance improvement [microform] : overview and future directions / Glenn Gilyard and Martín España.

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

  • Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2 [microform] / D. R. Boldman ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions [microform] / Richard P. Woodward and Christopher E. Hughes.

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

  • Ultra-high bypass ratio jet noise [microform] / John K.C. Low.

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

  • Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory [microform] / E. Carson Yates, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Measurements of store forces and moments and cavity pressures for a generic store in and near a box cavity at subsonic and transonic speeds [microform] / Robert L. Stallings ... [et al.].

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

  • Noise exposure reduction of advanced high-lift systems [microform] / Stephen W. Haffner.

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

  • Study of potential aerodynamic benefits from spanwise blowing at wingtip [microform] / Raymond E. Mineck.

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

  • Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils [microform] / Daryl L. Bonhaus, W. Kyle Anderson, and Dimitri J. Mavriplis.

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

  • A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines [microform] / Chung-Hua Wu.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • Noise impact of advanced high lift systems [microform] : contract NAS1-20103 / Kevin R. Elmer and Mahendra C. Joshi.

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

  • Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane [microform] / Dennis O. Allision and William G. Sewall.

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

  • 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

  • Pressure distributions from subsonic tests of a NACA 0012 semispan wing model [microform] / Zachary T. Applin.

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

  • The Kirchhoff formulas for moving surfaces in aeroacoustics [microform] : the subsonic and supersonic cases / F. Farassat.

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

  • Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration [microform] / W.P. Phillips and W.C. Engelund.

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

  • Subsonic dynamics of stardust sample return capsule [microform] / R.A. Mitcheltree and C.M. Fremaux.

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

  • Low-speed wind tunnel tests of two waverider configuration models [microform] / Robert J. Pegg, David E. Hahne, Charles E. Cockrell, Jr.

    • Text
    • Washington, D.C. : American Institute of Aeronautics and Astronautics : [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

  • Validation of vortex-lattice method for loads on wings in lift-generated wakes [microform] / Vernon J. Rossow.

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

  • Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60̊ angle of attack [microform] : contract NAS 3-26617 / Kevin R. Walsh ... [et al.].

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

  • Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft [microform] / W.G. Steenken ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Highlights of aeroacoustics research in the U.S.-1998 [microform] / Ganesh Raman, Dennis K. McLaughlin.

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

  • Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment [microform] / Donald Greer ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Cavity unsteady-pressure measurements at subsonic and transonic speeds [microform] / Maureen B. Tracy and E.B. Plentovich.

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

  • Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges [microform] / Julio Chu and James M. Luckring.

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

  • Static performance of six innovative thrust reverser concepts for subsonic transport applications [microform] : summary of the NASA Langley Innovative Thrust Reverser Test Program / Scott C. Asbury and Jeffrey A. Yetter.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22791

  • Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds [microform] / John E. Lamar ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26671

  • Flow unsteadiness effects on boundary layers [microform] / by Sreedhara V. Murthy.

    • Text
    • [Moffett Field, Calif. : NASA Ames Research Center, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60942

  • Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility [microform] / Peter F. Jacobs and Blair B. Gloss.

    • 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/LPS67806

  • Integrated application of active controls (IAAC) technology to an advanced subsonic transport project [microform] : test ACT system description / prepared for Langley Research Center under contract NAS1-15325.

    • Text
    • Hampton, Va. : National Aeronautics and Space Admininstration, Langley Research Center, [1983]
    • 1983

  • Integrated application of active controls (IAAC) technology to an advanced subsonic transport project [microform] : program review.

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

  • Effect of a rotating propeller on the separation angle of attack and distortion in ducted propeller inlets [microform] / D. R. Boldman, ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1992?]
    • 1992
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97761

  • Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles [microform] / H.C. Kao, P. L. Burstadt, and A. L. Johns.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • An experimental documentation of trailing-edge flows at high Reynolds number [microform] / P. R. Viswanath, J. W. Cleary, and H. L. Seegmiller.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
    • 1983

  • Method for the prediction of the installation aerodynamics of a propfan at subsonic speeds : user manual / B. Chandrasekaran.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo23588

  • Method for the prediction of the installation aerodynamics of a propfan at subsonic speeds [microform] : user manual / B. Chandrasekaran.

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

  • The Kirchhoff formulas for moving surfaces in aeroacoustics : the subsonic and supersonic cases / F. Farassat.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 1996.
    • 1996-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS67208

  • Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed / Gary E. Erickson.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2017.
    • 2017-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo81470

  • N+2 advanced low NOx combustor technology / John Herbon [and eleven oterhs].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2017.
    • 2017-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79534

  • Experimental and analytical evaluation of a composite honeycomb deployable energy absorber / Karen E. Jackson [and six others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33397

  • Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds / Gary E. Erickson.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo40586

  • Methods for estimating drag polars of subsonic airplanes.

    • Text
    • [Lawrence? Kan.], [1971]
    • 1971
    • 1 Item
    FormatCall NumberItem Location
    Text TL574.D7R67Off-site

  • 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

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