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  • Modeling the high speed research cycle 2B longitudinal aerodynamic database using multivariate orthogonal functions [microform] / E.A. Morelli and M.S. Proffitt.

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

  • Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation [microform] / Jensen Lin, Kenneth W. Iliff.

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

  • Application of two procedures for dual-point design of transonic airfoils [microform] / Raymond E. Mineck, Richard L. Campbell, and Dennis O. Allison.

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

  • Dynamic ground effects flight test of an F-15 aircraft [microform] / Stephen Corda ... [et al.].

    • 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

  • A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept [microform] / Bandu N. Pamadi.

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

  • Venusian atmospheric and Magellan properties from attitude cotrol data [microform] / Christopher A. Croom and Robert H. Tolson.

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

  • 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall [microform] / R.A. Piziali.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Dynamic stability instrumentation system (DSIS) [microform] / T.L. Jordan ... [et al.].

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

  • On the Lagrangian method for steady and unsteady flow [microform] / W.H. Hui and H.J. Van Roessel.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Rapport d'essais du profil CAST 10 en transition dʹeclenchʹee, effectuʹes dans la soufflerie transsonique cryogʹenique T2 en pr'esence de parois auto-adaptables [microform] = Report on tests of a CAST 10 airfoil with fiexed transition in the T2 transonic cryogenic wind tunnel with self-adaptive walls / A. Seraudie, A. Blanchard, J.F. Breil.

    • Text
    • Toulouse : Centre DʹEtudes et de Recherches de Toulouse, Dept., DʹEtudes et de Recherches en Aerothermodynamique ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Development of multiobjective optimization techniques for sonic boom minimization [microform] / Aditi Chattopadhyay, Johnny R. Narayan, Narayanan Pagaldipti.

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

  • Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data [microform] / Michael D. Messina.

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

  • An analysis for high speed propeller-nacelle aerodynamic performance prediction [microform] / T. Alan Egolf ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988.
    • 1988

  • Modern airfoil ice accretions [microform] / Harold E. Addy, Jr., Mark G. Potapczuk, and David W. Sheldon.

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

  • Determining the accuracy of aerodynamic model parameters estimated from flight test data [microform] / Eugene A. Morelli, Vladislav Klein.

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

  • Aeroelastic calculations using CFD for a typical business jet model [microform] / Michael D. Gibbons.

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

  • IPAC--Inlet Performance Analysis Code [microform] / Paul J. Barnhart.

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

  • An approach to the constrained design of natural laminar flow airfoils [microform] : a thesis ... / by Bradford Earl Green.

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

  • Rarefaction effects on Galileo probe aerodynamics [microform] / James N. Moss ... [et al.].

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

  • User's manual for FOMOCO utilities-force and moment computation tools for overset grids [microform] / William M. Chan, Pieter G. Buning.

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

  • Comparative results from a CFD challenge over a 2D three-element high-lift airfoil [microform] / Steven M. Klausmeyer, John C. Lin.

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

  • High-lift systems on commercial subsonic airliners [microform] / Peter K.C. Rudolph.

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

  • Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil [microform] / Dale Ashby.

    • Text
    • [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Comparison of several dissipation algorithms for central difference schemes [microform] / R.C. Swanson, R. Radespiel, E. Turkel.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Comparison of turbulence models for nozzle-afterbody flows with propulsive jets [microform] / William B. Compton III.

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

  • Two-dimensional high-lift aerodynamic optimization using neural networks [microform] / Roxana M. Greenman.

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

  • Experimental optimization methods for multi-element airfoils [microform] : final report / by Drew Landman and Colin P. Britcher, principal investigators ; submitted by the Old Dominion University Research Foundation.

    • 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, 1996]
    • 1996

  • Turbulence measurements on a flap-edge model [microform] : final report : NASA-Ames university consortium, NCC2-5140 / Patrick Moriarty ... [et al.].

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

  • Hypersonic pitching-moment shift for stardust reentry capsule forebody [microform] / William A. Wood.

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

  • Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept [microform] / David E. Hahne.

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

  • Study of the TRAC airfoil table computational system [microform] / Hong Hu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research 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

  • Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results [microform] / Jim A. Penland and Richard Hawkins.

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

  • Design and performance calculations of a propeller for very high altitude flight [microform] / L. Danielle Koch.

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

  • Sensitivity analysis for coupled aero-structural systems [microform] / Anthony A. Giunta.

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

  • Real-time method for estimating viscous forebody drag coefficients [microform] / Stephen A. Whitemore ... [et al.].

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

  • Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees [microform] / Ramadas K. Prabhu.

    • Text
    • Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS39080

  • Flight-measured laminar boundary-layer transition phenomena including stability theory analysis [microform] / Clifford J. Obara, Bruce J. Holmes.

    • 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

  • An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients [microform] : semiannual progress report, January 1991 - June 1991 / Leland A. Carlson.

    • Text
    • College Station, Tex. : Aerospace Engineering Dept., Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59910

  • An aerodynamic tradeoff study of the scissor wing configuration [microform] / Bruce P. Selberg, Kamran Rokhsaz, Clinton S. Housh.

    • Text
    • Rolla, Mo. : University of Missouri-Rolla ; [Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS63191

  • Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade [microform] / Kevin W. Noonan.

    • 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/LPS65498

  • Summary of longitudinal stability and control parameters as determined from space shuttle Challenger flight test data [microform] / William T. Suit.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS93085

  • A recontoured, upper surface designed to increase the maximum lift coefficient of a modified NACA 65 (0.82) (9.9) airfoil section [microform] / Raymond M. Hicks.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984

  • Use of adaptive walls in 2D tests [microform] / J.P. Archambaud and J.P. Chevallier.

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

  • Flight measurements of hinged-plate wing-spoiler hinge moments [microform] / Emmett B. Fry.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99705

  • Unsteady aerodynamic characterization of a military aircraft in vertical gusts [microform] / A. Le Bozec and J.L. Cocquerez.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1985]
    • 1985

  • An aerodynamic analysis computer program and design notes for low speed wing flap systems [microform] / Harry W. Carlson and Kenneth B. Walkley ; prepared for Langley Research Center under contract NAS1-16000.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104929

  • Potential benefits of magnetic suspension and balance systems / Pierce L. Lawing, David A. Dress, and Robert A. Kilgore.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112209

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