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  • Crossflow stability and transition experiments in swept-wing flow [microform] / J. Ray Dagenhart, William S. Saric.

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

  • LWC and temperature effects on ice accretion formation on swept wings at glaze ice conditions [microform] / Mario Vargas, Eli Reshotko.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; [Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service, distributor, 2000]
    • 2000

  • Optimum aerodynamic design via boundary control [microform] / Antony Jameson.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Vortex instabilities in 3D boundary layers [microform] : the relationship between Görtler and crossflow vortices / Andrew P. Bassom nad Philip Hall.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • The NASA Langley laminar-flow-control experiment on a swept supercritical airfoil [microform] : basic results for slotted configuration / Charles D. Harris ... [et al.].

    • 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

  • A spectrally accurate boundary-layer code for infinite swept wings [microform] / C. David Pruett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1994

  • Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet [microform] / Colin S. Bidwell and Stanley R. Mohler.

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

  • Multivariable control of a forward swept wing aircraft [microform] / Wilma W. Quinn.

    • Text
    • [Washington, D.C.?] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Aerodynamic shape optimization of wing and wing-body configurations using control theory [microform] / James Reuther and Antony Jameson.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A theory for lateral wing-tip blowing [microform] / by D. Tavella and L. Roberts.

    • Text
    • [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Wave interactions in a three-dimensional attachment line boundary layer [microform] / Phillp Hall, Sharon O. MacKerrell.

    • Text
    • Hampton, VA : NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • 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

  • Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing [microform] / Dhanvada M. Rao.

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

  • Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] : final report / Stephen W.D. Wolf.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Experimental investigation of the inlet deflector configuration variation in the flow field at mach 1.9 [microform] : final report / by Kyu C. Hwang, Surrendra N. Tiwari, and Stanley J. Miley.

    • Text
    • Norfolk, VA : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data [microform] : final report / by R.C. Potter and C.P. van Dam.

    • Text
    • Davis, CA : Dept. of Mechanical and Aeronautical Engineering, University of California ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel [microform] : final report / submitted by William S. Saric.

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

  • Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes [microform] / Gregory M. Catlin, Brian E. McGrath.

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

  • A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region [microform] / Edward C. Polhamus.

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

  • Wing leading edge joint laminar flow tests [microform] / Aaron Drake ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Effects of suction on swept-wing transition [microform] : final technical report on NASA-Langley award # NAG-1-194, 16 December 1995 to 31 March 1998 / by William S. Saric.

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

  • Distributed-roughness effects on stability and transition in swept-wing boundary layers [microform] : annual technical report ... NASA-Langley cooperative agreement # NCC-1-194 and the Boeing Company contract #ZA0078, during 5/17/96-12/31/96 / submitted by Ruben B. Carrillo, Jr.; Mark S. Reibert; William S. Saric (principal investigator).

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

  • Physical mechanisms of glaze ice scallop formations on swept wings [microform] / Mario Vargas, Eli Reshotko.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Natural rolling responses of a delta wing in transonic and subsonic flows [microform] / Margaret A. Menzies and O. Kandil.

    • Text
    • Reston, Va. : American Institute of Aeronautics and Aeronautics ; [Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Unsteady, transonic flow around delta wings undergoing coupled and natural modes response : a multidisciplinary problem / by Margaret Anne Menzies ; a dissertation submitted to the Faculty of Old Dominion University in partial fulfillment of the requirement for the degree of Doctor of Philosophy, Aerospace Engineering, Old Dominion University.

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

  • Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing [microform] / Sheryll Goecke Powers and Lannie D. Webb.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Boundary layer transition in the leading edge region of a swept cylinder in high speed flow [microform] / Colin P. Coleman.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Swept-wing receptivity studies using distributed roughness [microform] : annual technical report / William S. Saric.

    • Text
    • Tempe, AZ : Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Parametric experimental study of the formation of glaze ice shapes on swept wings [microform] / Mario Vargas, Eli Reshotko.

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

  • Natural laminar flow flight experiments on a swept wing business jet [microform] : boundary layer stability analyses / R. A. Rozendaal.

    • 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

  • Navier-Stokes simulation of the crossflow instability in swept-wing flows [microform] : a final report to National Aeronautics and Space Administration, Langley Research Center ; submitted by Helen L. Reed.

    • Text
    • Tempe, AZ : Dept. of Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68330

  • Swept wing ice accretion modeling [microform] / Mark G. Potapczuk and Colin S. Bidwell ; prepared for the 28th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 8-11, 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/LPS67499

  • Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing [microform] / Samuel J. Scott, Oran W. Nicks, and P. K. Imbrie.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • On the stability of an infinite swept attachment line boundary layer [microform] / P. Hall, M. R. Malik, D. I. A. Poll.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
    • 1984

  • ALESEP, Part II [microform] : a computer program for the analysis of leading edge separation bubbles on infinite swept wings / R.L. Davis and J.E. Carter.

    • Text
    • East Hartford, CT : United Technologies Research Center ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986

  • Subsonic flow investigations on a cranked wing designed for high maneuverability / Dhanvada M. Rao.

    • 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/gpo27947

  • Subsonic flow investigations on a cranked wing designed for high maneuverability [microform] / Dhanvada M. Rao.

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

  • Further evaluation of scaling methods for rotorcraft icing / Jen-Ching Tsao, Richard E. Kreeger.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo30594

  • Calculation of vortex-flap aerodynamic characteristics / by C. Edward Lan and C.C. Hsing.

    • Text
    • Lawrence, Kansas : Flight Research Laboratory, Department of Aerospace Engineering, the University of Kansas ; [Washington, D.C.] : [National Aeronautics and Space Administration], 1985.
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo46526

  • Calculation of vortex-flap aerodynamic characteristics / by C. Edward Lan and C.C. Hsing.

    • Text
    • Lawrence, Kansas : Flight Research Laboratory, Department of Aerospace Engineering, the University of Kansas ; [Washington, D.C.] : [National Aeronautics and Space Administration], 1985.
    • 1985

  • Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove / Trong T. Bui.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, January 2014.
    • 2014-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50966

  • Aerodynamic classification of swept-wing ice accretion / Jeff M. Diebold, Andy P. Broeren, Michael B. Bragg.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55297

  • Swept-wing ice accretion characterization and aerodynamics / Andy P. Broeren [and five others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55295

  • Novel control effectors for truss braced wing / Edward V. White, Rakesh K. Kapania, Shiv Joshi.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2015.
    • 2015-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62865

  • Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects / Andy P. Broeren [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2017.
    • 2017-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo85650

  • LWC and temperature effects on ice accretion formation on swept wings at glaze ice conditions / Mario Vargas, Eli Reshotko.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2000.
    • 2000-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo85944

  • Aerodynamic classification of swept-wing ice accretion / Andy P. Broeren, Jeff M. Diebold and Michael B. Bragg.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2013]
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo39828

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