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  • Wake geometry measurements and analytical calculations on a small-scale rotor model [microform] / Terence A. Ghee ... [et al.].

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

  • Determination of the pressure drag of airfoils by integration of surface pressures [microform] / Williams H. Phillips.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Effect of acoustic excitation on stalled flows over an airfoil [microform] / K.B.M.Q. Zama.

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

  • Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes [microform] / William L. Kleb, John T. Batina, Marc H. Williams.

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

  • A two dimensional study of rotor/airfoil interaction in hover [microform] / by Chyang S. Lee.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Palo Alto, Calif.] : Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft) [microform] / Edwin J. Saltzman, John W. Hicks.

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

  • Development of a turbomachinery design optimization procedure using a multiple-parameter nonlinear perturbation method [microform] / Stephen S. Stahara.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1984.
    • 1984

  • Study by double exposure holography of the three-dimensional character of the flow around an airfoil profile in a wind tunnel [microform] / G. Heid and M. Stanislas.

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

  • 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

  • Control of unsteady separated flow associated with the dynamic stall of airfoils [microform] : final report, 95-09 / M.C. Wilder.

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

  • A comparison of design variables for control theory based airfoil optimization [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

  • 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

  • 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

  • Control theory based airfoil design for potential flow and a finite volume discretization [microform] / J. Reuther and A. Jameson.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1995

  • Annual progress report ... entitled An experimental investigation of the flow physics of high-lift systems, for the period March-December 1995 [microform] / by Flint O. Thomas and R.C. Nelson.

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

  • Improving CPA-TSD steady pressure solutions through airfoil slope modification [microform] / Kent F. Mitterer ... [et al.].

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

  • Development and testing of airfoils for high-altitude aircraft [microform] : final report / principal investigator, Mark Drela.

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

  • PROFILE [microform] : airfoil geometry manipulation and display : user's guide / Leslie Collins, David Saunders.

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

  • Aerodynamics of heat exchangers for high-altitude aircraft [microform] / Mark Drela.

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

  • Assessment of dual-point drag reduction for an executive-jet modified airfoil section [microform] / Dennis O. Allison and Raymond E. Mineck.

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

  • Computer program to obtain ordinates for NACA airfoils [microform] / Charles L. Ladson ... [et al.].

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

  • The development of a tool for semi-automated generation of structured and unstructured grids about isolated rotorcraft blades [microform] / by Ramakrishnan Shanmugasundaram, Javier A. Garriz, and Jamshid A. Samareh.

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

  • A feasibility study to control airfoil shape using THUNDER [microform] / Jennifer L. Pinkerton and Robert W. Moses.

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

  • 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

  • Application of a third order upwind scheme to viscous flow over clean and iced wings [microform] : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV / A. Bangalore, N. Phaengsook and L.N. Sankar.

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

  • Airfoil dynamic stall and rotorcraft maneuverability [microform] / William G. Bousman.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23428

  • Compressible flows with periodic vortical disturbances around lifting airfoils [microform] / James R. Scott.

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61870

  • Final design proposal [microform] : the MANTA : an RPV designed to investigate forces and moments on a lifting surface / [Kevin Bryan ... et al.].

    • Text
    • Notre Dame, IN : Dept. of Aerospace and Mechanical Engineering, University of Notre Dame ; [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/LPS63197

  • Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil [microform] / David E. Hahne and Frank L. Jordan, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67812

  • Adaptive grid embedding for the two-dimensional flux-split Euler equations [microform] / by Gary Patrick Warren.

    • Text
    • Mississippi State, Miss. : Mississippi State University, Dept. of Aerospace Engineering, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69258

  • Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model [microform] / Zachary T. Applin and Garl L. Gentry, 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], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68609

  • Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel [microform] / William G. Johnson, Jr., and Acquilla S. Hill.

    • 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
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85654

  • Three-dimensional effects on airfoils [microform] / J.P. Chevallier.

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

  • Design procedures for compressor blades [microform] / H. Starken.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, [1983]
    • 1983

  • Profile design for wings and propellers [microform] / A. Quast and K.H. Horstmann.

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

  • An exploratory investigation of a slotted, natural-laminar-flow airfoil / Dan M. Somers.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo27796

  • Validation of 3-D ice accretion measurement methodology for experimental aerodynamic simulation / Andy P. Broeren [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2015.
    • 2015-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo61931

  • Computer program to obtain ordinates for NACA airfoils / Charles L. Ladson [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65379

  • A feasibility study to control airfoil shape using THUNDER / Jennifer L. Pinkerton and Robert W. Moses.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1997.
    • 1997-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65617

  • Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses / by Charles D. Harris.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, April 1972.
    • 1972-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65338

  • Airfoil dynamic stall and rotorcraft maneuverability / William G. Bousman.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, July 2000.
    • 2000-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS23428

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