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  • Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms [microform] / Kevin J. Kjerstad ... [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

  • Low-speed stability-and-control and ground-effects measurements on the industry reference high speed civil transport [microform] / Guy T. Kemmerly ... [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

  • Effect of control surface mass unbalance on the stability of a closed-loop active control system [microform] / E. Nissim.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1989.
    • 1989

  • Project HyBuJet [microform] : final report / student authors, T. Ramsay ... [et al.].

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

  • Active load control during rolling maneuvers [microform] / Jessica A. Woods-Vedeler, Anthony S. Pototzky, and Sherwood T. Hoadley.

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

  • 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

  • Improved control surface actuator [microform] / inventor, Gerhard E. Seidel.

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

  • Launch vehicle flight control augmentation using smart materials and advanced composites (CDDF project 93-05) [microform] / C. Barret.

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

  • A concept for adaptive performance optimization on commercial transport aircraft [microform] / Michael R. Jackson, and Dale F. Enns.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Numerical study of steady and unsteady canard-wing-body aerodynamics [microform] / Eugene L. Tu.

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

  • Laser scanning system for pressure and temperature paints [microform] : final report, NASA NCC2-5115 / John Sullivan.

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

  • Navier-Stokes computations on full wing-body configuration with oscillating control surfaces [microform] / Shigeru Obayashi, Ing-Tsau Chiu, Guru P. Guruswamy.

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

  • Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer [microform] / Alan Celić, Gregory G. Zilliac.

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

  • Microfabricated ice-detection sensor [microform] / Russell G. DeAnna, Mehran Mehregany and Shuvo Roy.

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

  • Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft [microform] / Robert Navarro.

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

  • Instability and transition of flow at, and near, an attachment-line [microform] : including control by surface suction / A. Smith and D.I.A. Poll.

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

  • Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates [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, [1999]
    • 1999

  • 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

  • Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations [microform] / Robert M. Bennett and Charlotte E. Walker.

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

  • Thermal control surfaces experiment [microform] / D.R. Wilkes.

    • Text
    • [Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft [microform] / Vladislav Klein ... [et al.].

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

  • Further investigations of control surface seals for the X-38 re-entry vehicle [microform] / Patrick H. Dunlap ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26910

  • Investigations of control surface seals for re-entry vehicles [microform] / Patrick H. Dunlap ... [et al.] ; [prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002

  • Investigations of control surface seals for re-entry vehicles [microform] / Dunlap, Patrick H. ; [prepared for 39th Joint Propulsion Conference and Exhibit ; cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS36329

  • Testing and optimization of electrically conductive spacecraft coatings [microform] / R.J. Mell, G.E. Wertz.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS39081

  • Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations [microform] / Robert W. Hess, F. W. Cazier, Jr., and Eleanor C. Wynne.

    • 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

  • On orbit surfacing of thermal control surfaces [microform] : monthly progress report #7 / prepared for George C. Marshall Space Flight Center.

    • Text
    • Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [1984]
    • 1984

  • Wind-tunnel investigation of a full-scale canard-configured general aviation airplane [microform] / Long P. Yip.

    • 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/LPS54941

  • Prediction of forces and moments for flight vehicle control effectors [microform] / M. Maughmer ... [et al.].

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 2 Resources

    Available Online

    See All Available Online Resources

  • A computer module used to calculate the horizontal control surface size of a conceputal aircraft design [microform] / principal investigator, Doral R. Sandlin ; student assistant, Stephen Mark Swanson..

    • 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, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69281

  • Experimental study of fluid deicing system in the NASA Icing Research Tunnel [microform].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983

  • Transonic steady- and unsteady-pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces [microform] / Maynard C. Sandford, Rodney H. Ricketts, and F.W. Cazier, Jr.

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

  • Subsonic and transonic pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces [microform] / Maynard C. Sandford, Rodney H. Ricketts, and Judith J. Watson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, [1981]
    • 1981
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97353

  • Steady- and unsteady-pressure measurements on a supercritical wing model with oscillating control surfaces at subsonic and transonic speeds [microform] / Maynard C. Sandford and Rodney H. Ricketts.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983.
    • 1983

  • High-temperature modal survey of a hot-structure control surface / Natalie D. Spivey.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24035

  • Evaluation of brushing as a lunar dust mitigation strategy for thermal control surfaces / James R. Gaier ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24330

  • Thermal optical properties of lunar dust simulants and their constituents / James R. Gaier, Shaneise Ellis, and Nichole Hanks.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24332

  • Implications of adhesion studies for dust mitigation on thermal control surfaces / James R. Gaier and Stephen P. Berkebile.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo26337

  • Evaluation of surface modification as a lunar dust mitigation strategy for thermal control surfaces / James R. Gaier ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27067

  • Adhesion between volcanic glass and spacecraft materials in an airless body environment / Stephen Berkebile, Kenneth W. Street, Jr., and James R. Gaier ; prepared for the 3rd Atmospheric and Space Environments Conference sponsored by the American Institute of Aeronautics and Astronautics, Honolulu, Hawaii, June 27-30, 2011.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo27507

  • Advanced composite stabilizer for Boeing 737 aircraft : fifth quarterly technical progress report, 19 July 1978 through 18 October 1978.

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

  • A non-cut cell immersed boundary method for use in icing simulations / Christian M. Sarofeen and Ralph W. Noack, Richard E. Kreeger.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
    • 2013-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo47644

  • Advanced composite stabilizer for Boeing 737 aircraft.

    • Text
    • Seattle, Washington : Boeing Commercial Airplane Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985?]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo35016

  • Computations on wings with full-span oscillating control surfaces using Navier-Stokes equations / Guru P. Guruswamy.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, May 2013.
    • 2013-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53310

  • Rapid state space modeling tool for rectangular wing aeroservoelastic studies / Peter M. Suh, Howard J. Conyers, Dimitri N. Mavris.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, September 2015.
    • 2015-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65159

  • Microfabricated ice-detection sensor / Russell G. DeAnna, Mehran Mehregany and Shuvo Roy.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72582

  • Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft / Vladislav Klein [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1997.
    • 1997-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo78975

  • Adhesion in a vacuum environment and its implications for dust mitigation techniques on airless bodies / Stephen Berkebile and James R. Gaier.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo33007

  • Rotating rig development for droplet deformation/breakup and impact induced by aerodynamic surfaces / A. Feo, M. Vargas, A Sor.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo37252

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