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  • A generalized wall function [microform] / Tsan-Hsing Shih ... [et al.].

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

  • A wall interference assessment/correction system [microform] : final report, June 1991 - June 1994 / C.F. Lo, principal investigator.

    • Text
    • Tullahoma, TN : Center for Space Transportation and Applied Research ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Computation of turbulent boundary layers employing the defect wall-function method [microform] / Douglas L. Brown.

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

  • Development of a near-wall Reynolds-stress closure based on the SSG model for the pressure strain [microform] / R.M.C. So ... [et al.].

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

  • A laser Doppler velocimeter approach for near-wall three-dimensional turbulence measurements [microform] / D.A. Johnson and J.D. Brown.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • 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

  • Non-linear evolution of a second mode wave in supersonic boundary layers [microform] / Gordon Erlebacher, M.Y. Hussaini.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Flow boiling with enhancement devices for cold plate coolant channel design [microform] : semiannual report / by Ronald D. Boyd, Sr.

    • Text
    • Prairie View, TX : College of Engineering, Prairie View A&M University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Modeling of wall-bounded complex flows and free shear flows [microform] / Tsan-Hsing Shih, Jiang Zhu, John L. Lumley.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Effects of artificial viscosity on the accuracy of high-Reynolds-number [kappa-epsilon] turbulence model [microform] / Tawit Chitsomboon.

    • Text
    • Cleveland, Ohio : NASA, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Turbulence modelling of flow fields in thrust chambers [microform] : final technical report for the period June 10, 1991 through September 13, 1992 / prepared by C.P. Chen, Y.M. Kim, H.M. Shang.

    • Text
    • [Huntsville, Ala.] : Research Institute, the University of Alabama in Huntsville ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • 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 near wall flow parameters in the blade end-wall corner region [microform] / Rakesh K. Bhargava and Rishi S. Raj.

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

  • Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing [microform] / A.V. Murthy.

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

  • Supersonic quiet-tunnel development for laminar-turbulent transition research [microform] : final report for NASA Langley grant NAG-1-1607 / Steven P. Schneider.

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

  • Transonic interference reduction by limited ventilation wall panels [microform] / John D. Lee.

    • Text
    • Cleveland, Ohio : Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Scramjet sidewall burning, preliminary shock tunnel results, NASA contract no. NAGW-674 [microform] / by R.G. Morgan ... [et al.].

    • Text
    • [Brisbane, Australia] : University of Queensland, Dept. of Mechanical Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Low Reynolds number two-equation modeling of turbulent flows [microform] / V. Michelassi and T.-H. Shih.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor [microform] / Kenneth L. Suder and Mark L. Celestina.

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

  • Flow in serpentine coolant passages with trip strips [microform] : technical progress narrative report, reporting period September 1, 1995 to September 30, 1995 / D.G.-N. Lee.

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

  • Instrumentation development for study of Reynolds analogy in reacting flows [microform] / D.J. DeTurris.

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

  • Endwall heat transfer measurements in a transonic turbine cascade [microform] / P.W. Giel ... [et al.].

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

  • Endwall heat transfer measurements in a transonic turbine cascade [microform] / P.W. Giel ... [et al.].

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

  • The physics of turbulence in the boundary layer [microform] : final report ... NASA grant NAG-1-1610 / Stephen Kline and Brian Cantwell.

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

  • A near-wall Reynolds-stress closure without wall normals [microform] : final report ... under grant number NAG-1-1772 / S.P. Yuan and R.M.C. So.

    • Text
    • Tempe, Ariz. : College of Engineering and Applied Sciences, Arizona State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Predicted turbine heat transfer for a range of test conditions [microform] / R.J. Boyle and B.L. Lucci.

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

  • The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel [microform] / Norbert Ulbrich.

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

  • Description of panel method code ANTARES [microform] / Norbert Ulbrich.

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

  • Analysis of transitional separation bubbles on infinite swept wings [microform] / R. L. Davis and J. E. Carter.

    • 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

  • Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall [microform] / Joel L. Everhart and Percy J. Bobbitt.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60769

  • Development of a defect stream function, law of the wall/wake method for compressible turbulent boundary layers [microform] / Richard A. Wahls.

    • 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/LPS61721

  • Near-wall modelling of compressible turbulent flows [microform] : a semi-annual progress report / by Ronald M.C. So.

    • Text
    • Tempe, Ariz. : Arizona State University ; Hampton, VA : NASA Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64230

  • A critical evaluation of two-equation models for near wall turbulence [microform] / Charles G. Speziale, Ridha Abid, E. Clay Anderson.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69476

  • 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

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

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

  • 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

  • Semiempirical methods for computing turbulent flows [microform] / I.A. Belov, I.P. Ginzburg.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986

  • Corrections for attached sidewall boundary-layer effects in two-dimensional airfoil testing [microform] / A.V. Murthy.

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

  • An efficient parallel algorithm for the simulation of three-dimensional compressible transition on a 20 processor Flex/32 multicomputer [microform] / G. Erlebacher, Shahid H., Bokhari, M. Y., Hussaini.

    • Text
    • Hampton, Va. : Universities Space Research Association, Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1987]
    • 1987

  • An experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor / Reid A. Berdanier and Nicole L. Key.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.
    • 2015-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65196

  • Predicted turbine heat transfer for a range of test conditions / R.J. Boyle and B.L. Lucci.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70711

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