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  • Study of the application of separation control by unsteady excitation to civil transport aircraft [microform] / J.D. McLean ... [et al.].

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

  • Analysis of aerospike plume induced base-heating environment [microform] / T.-S. Wang.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Active control of flow separation over an airfoil [microform] / S.S. Ravindran.

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

  • Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [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

  • Control of low-speed turbulent separated flow over a backward-facing ramp [microform] / by John C. Lin.

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

  • A steadying effect of acoustic excitation on transitory stall [microform] / K.B.M.Q. Zaman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1991]
    • 1991

  • A computionally efficient modelling of laminar separation bubbles [microform] : semi-annual status report, June 1988 - January 1989 for NASA grant NAG-1-778 / Paolo Dini and Mark D. Maughmer.

    • Text
    • University Park, PA : Dept. of Aerospace Engineering, Pennsylvania State University ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Control of unsteady separated flow associated with the dynamic stall of airfoils [microform] / M.C. Wilder.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Numerical simulation of the SOFIA flowfield [microform] / Stephen P. Klotz.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Control of separated flow past a cylinder using tangential wall jet blowing [microform] / by Sejong Oh and Leonard Roberts.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Numerical simulation of helicopter engine plume in forward flight [microform] : final report cooperative agreement #NCC2-5061 / Arsenio C.B. Dimanlig, Cornelis P. van Dam, Earl P.N. Duque.

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

  • Unsteady three-dimensional flow separation [microform] / W.H. Hui.

    • Text
    • Waterloo, Ont. : University of Waterloo Research Institute ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Numerical investigation of the effects of icing on fixed and rotary wing aircraft [microform] : progress report for the period January 1, 1992-June 30, 1992 / prepared by L.N. Sankar.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • A transport model of the turbulent scalar-velocity [microform] : status report / R.S. Amano and P. Goel and J.C. Chai.

    • Text
    • Milwaukee, Wis. : Dept. of Mechanical Engineering, University fo Wisconsin--Milwaukee ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows [microform] / Khaled S. Abdol-Hamid, B. Lakshmanan, John R. Carlson.

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

  • Third-moment closure of turbulence for predictions of separating and reattaching shear flows [microform] : final report on "A study of Reynolds-Stress Closure Model" / by R.S. Amano, principal investigator and Pankaj Goel, research assistant.

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

  • Formation of asymmetric separated flow past slender bodies of revolution at large angles of attack [microform].

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

  • SSME main combustion chamber and nozzle flowfield analysis [microform] : final report / prepared by Richard C. Farmer ... [et al.].

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

  • Numerical investigation of the effects of icing on fixed and rotary wing aircraft [microform] : progress report for the period January 1, 1992 - June 30, 1992 / prepared by L.N. Sankar.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • A study of the second and third order closure models of turbulence for prediction of separated shear flows [microform] / by R.S. Amano.

    • Text
    • Milwaukee, Wis. : Dept. of Mechanical Engineering, University of Wisconsin--Milwaukee ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • The structure of separated flow regions occurring near the leading edge of airfoils, including transition [microform] : semi-annual status report, February 1986-July 1986 / Thomas J. Mueller, principal investigator.

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

  • Simulation of brush insert for leading-edge-passage convective heat transfer [microform] / R.C. Hendricks ... [et al.].

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

  • Turbulence modeling [microform] / Jorge E. Bardina.

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

  • Application of viscous-inviscid interaction methods to transonic turbulent flows [microform] / by D. Lee, R.H. Pletcher.

    • Text
    • [Ames, Iowa] : Iowa State University. Engineering Research Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • A turbulence model for the NPARC code [microform] / J. Zhu and T.H. Shih.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An investigation of bleed configurations and their effect on shock wave/boundary layer interactions [microform] : final report / Awatef Hamed, principal investigator.

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

  • Boundary layer transition studies [microform] : November 1990 to February 1995 / Jonathan H. Watmuff.

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

  • An experimental study of a turbulent boundary layer in the trailing edge region of a circulation-control airfoil [microform] / Jeff Brown.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1995]
    • 1995

  • Implementation of a two-equation K-[omega] turbulence model in NPARC [microform] / Dennis A. Yoder and Nicholas J. Georgiadis, Paul D. Orkwis.

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

  • Evaluation of F/A-18A HARV inlet flow analysis with flight data [microform] / C. Frederic Smith ... [et al.].

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

  • PARC3D calculations of the F/A-18A HARV inlet vortex generators [microform] / Steve D. Podleski.

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

  • Final report on study of organized structures in the post-stall flow over wings [microform] / Steven Yon; Joseph Katz, principal investigator; James Ross, principal investigator.

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

  • Fully nonlinear Görtler vortices in constricted channel flows and their effect on the onset of separation [microform] / James P. Denler, Philip Hall.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade [microform] / Daniel H. Buffum ... [et al.].

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

  • An experimental study of a separated/reattached flow behind a backward-facing step. Re[subscript h] = 37,000 [microform] / Srba Jovic.

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

  • Experimental investigation of plume-induced flow separation on the National Launch System 1¹/₂-stage launch vehicle [microform] : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994, Reno, NV / A. Springer.

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

  • 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

  • Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] / John W. Edwards.

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

  • Study of the unsteady flow features on a stalled wing [microform] / S. Yon and J. Katz.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Enhanced line integral convolution with flow feature detection [microform] : NAS technical report NAS-96-007 / Arthur Okada, David Lane.

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

  • Evaluation of turbulence models for unsteady flows of an oscillating airfoil [microform] / G.R. Srinivasan, J.A. Ekaterinaris, and W.J. McCroskey.

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

  • Study of boundary layer development in a two-stage low-pressure turbine [microform] / Daniel J. Dorney ... [et al.].

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

  • A final report on the NASA grant NAG-1-1612 of large-vortex capture by a wing at very high angles of attack [microform] / prepared by J.M. Wu ... [et al.].

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

  • Computation of separated and unsteady flows with one- and two-equation turbulence models [microform] : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV / J.A. Ekaterinaris and F.R. Menter.

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

  • Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] : EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996 / John W. Edwards.

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

  • Assessment of an unstructured-grid method for predicting 3-D turbulent viscous flows [microform] : 34th Aerospace Sciences Meeting, January 15-18, 1996/Reno, Nevada / Neal T. Frink.

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

  • Closed-loop separation control using oscillatory flow excitation [microform] / Brian G. Allan ... [et al.] ; [prepared for ... under contract NAS1-97046].

    • Text
    • Hampton, Va. : ICASE, National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2000]
    • 2000

  • Summary of EASM turbulence models in CFL3D with validation test cases [microform] / Christopher L. Rumsey and Thomas B. Gatski.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS51551

  • Enhanced design of turbo-jet LPT by separation control using phased plasma actuators [microform] / Thomas C. Corke and Flint O. Thomas.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Administration ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55124

  • Demonstration of separation delay with glow-discharge plasma actuators [microform] / Lennart S. Hultgren and David E. Ashpis.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, Md. : Available from the NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55252

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