Research Catalog

  • Low speed windtunnel measurements on a two-dimensional flapped wing model using tunnel wall boundary layer control at the wing-wall junctions / by D.M. de Vos.

    • Text
    • [Amsterdam] : Nationaal Lucht- en Ruimtevaartlaboratorium, 1973.
    • 1973
    • 1 Item
    FormatCall NumberItem Location
    Text JSF 91-953Offsite
  • Initial adaptation testing of the bidimensionally self-adapting wall of the French T2 windtunnel, around a three-dimensional object [microform] / J.P. Archambaud ... [et al.].

    • Text
    • Washington DC : National Aeronautics and Space Administration, [1986]
    • 1986-1986
  • Mass flux similarity for slotted transonic-wind-tunnel walls [microform] / Joel L. Everhart, Suresh H. Goradia.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991
  • Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques [microform] / Raymond E. Mineck.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992
  • Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel [microform] / G.S. Manuel and John K. Molloy, P. Stephen Barna.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992
  • Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel [microform] / Raymond E. Mineck and Acquilla S. Hill.

    • 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], 1990.
    • 1990
  • Adaptive wind tunnel walls [microform] : a selected, annotated bibliograpy / Marie H. Tuttle, Raymond E. Mineck.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
    • 1986
  • Slotted-wall flow-field measurements in a transonic wind tunnel [microform] / Joel L. Everhart, William B. Igoe, and Stuart G. Flechner.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991
  • Computation of wind tunnel wall effects for complex models using a low-order panel method [microform] / Dale L. Ashby and Scott H. Harris.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • A method for the modelling of porous and solid wind tunnel walls in computational fluid dynamics codes [microform] / by Thomas John Beutner.

    • Text
    • [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; Stanford, CA : Stanford University , Dept. of Aeronautics and Astronautics ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • An engineering study of hybrid adaptation of wind tunnel walls for three dimensional testing [microform] / C.E. Brown, K.M. Kalumuck, and D.N. Waxman.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • Theoretical and experimental studies of the transonic flow field and associated boundary conditions near a longitudinally-slotted wind-tunnel wall [microform] / by Joel Lee Everhart.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988
  • Adaptive wall technology for minimization of wall interferences in transonic wind tunnels [microform] / Stephen W.D. Wolf.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988.
    • 1988
  • Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel [microform] / S. Balakrishna, W. Allen Kilgore, and A.V. Murthy.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
  • Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack [microform] / Crawford F. Smith.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • A wall interference assessment/correction system [microform] / Dr. C.F. Lo, principal investigator.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • An experimental study of an adaptive-wall wind tunnel [microform] / by Zeki Celik and Leonard Roberts.

    • Text
    • Stanford, CA : Joint Institute for Aeronautics and Acoustics, Stanford University, Dept. of Aeronautics and Astronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988
  • Derivation of jack movement influence coefficients as a basis for selecting wall contours giving reduced levels of interference in flexible walled test sections [microform] / M.J. Goodyer.

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
    • 1985
  • The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel [microform] / Mark C. Lewis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
    • 1985
  • Investigation of water droplet trajectories within the NASA icing research tunnel [microform] / Andrew L. Reehorst and Mounir Ibrahim.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Assessment of two-equation turbulence models for transonic flows [microform] / Florian R. Menter, Christopher L. Rumsey.

    • Text
    • Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Computer simulation of a wind tunnel test section with discrete finite-length wall slots [microform] / William B. Kemp, Jr.

    • 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
  • A wall interference assessment/correction interface measurement system for the NASA-ARC 12-FT PWT [microform] : final memorandum report.

    • Text
    • [Tullahoma, Tenn. : The University of Tennessee-Calspan Center Aerospace Research (CAR) ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61599
  • Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer [microform] / by M.K. Bhat, A.D. Vakili, and J.M. Wu.

    • Text
    • Tullahoma, TN : The University of Tennessee Space Institute ; [Moffett Field, CA] : NASA Ames Research Center ; [Springfield, VA :: For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64316
  • A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel [microform] / Edward T. Schairer and George Lee, T. Kevin McDevitt.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70036
  • Study of the integration of wind tunnel and computational methods for aerodynamic configurations [microform] / Lindsay E. Browne and Dale L. Ashby.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70437
  • Reverberation effects on directionality and response of stationary monopole and dipole sources in a wind tunnel [microform] / Kenneth J. Baumeister.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1985]
    • 1985
  • A cooperative program to stimulate student involvement through the MIT undergraduate research opportunity program [microform] : final report / principal investigators, Eugene E. Covert, ... [et al.].

    • Text
    • Cambridge, Mass. : Massachusetts Institute of Technology, Dept. of Aeronautics & Astronautics ; Hampton, Va. : NASA Langley Research Center, [1984]
    • 1984
  • Tests on a CAST 7 two-dimensional airfoil in a self-streamlining test section [microform] / M.J. Goodyer.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley 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
  • Flexwall [microform] : a computer program for predicting the wall modifications for two-dimensional, solid, adaptive-wall wind tunnels / Joel L. Everhart.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983
  • Laminarization of a boundary layer in a supersonic nozzle by cooling of the surface [microform] / V.P. Maksimov and A.A. Maslov.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983
  • Effect of ground and/or ceiling planes on thrust of rotors in hover [microform] / Vernon J. Rossow.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104581
  • "Flexiwall 3 SO" [electronic resource] : a seond-order predictive strategy for rapid wall adjustment in two-dimensional compressible flow / Michael Judd.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113574
  • An evaluation of three experimental processes for two-dimensional transonic tests [electronic resource] / Gennaro Zuppardi.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113662
  • "Flexiwall 3 SO" [microform] : a seond-order predictive strategy for rapid wall adjustment in two-dimensional compressible flow / Michael Judd.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113574
  • An evaluation of three experimental processes for two-dimensional transonic tests [microform] / Gennaro Zuppardi.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113662
  • Modifications to Langley 0.3-m TCT adaptive wall software for heavy gas test medium. Phase 1 studies [microform] / A. V. Murthy.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1992]
    • 1992
  • Subsonic wind tunnel wall corrections, by H. C. Garner [and others] Editor: H. C. Garner.

    • Text
    • [Paris, North Atlantic Treaty Organization] 1966.
    • 1966
    • 1 Item
    FormatCall NumberItem Location
    Text 92519.891Off-site
  • Wind tunnel corrections for high angle of attack models.

    • Text
    • Nuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research & Development, c1981.
    • 1981
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-692Off-site
  • Subsonic wind tunnel wall corrections, by H.C. Garner [and others] editor, H.C. Garner.

    • Text
    • [Paris], [North Atlantic Treaty Organization] 1966.
    • 1966
    • 1 Item
    FormatCall NumberItem Location
    Text 92519.891Off-site
  • Wind tunnel corrections for high angle of attack models.

    • Text
    • Nuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research & Development, c1981.
    • 1981
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-692Off-site

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