Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions [microform] / principle investigators: William J. Devenport, Stewart A.L. Glegg.

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

  • Numerical simulation of the edge tone phenomenon [microform] / N.S. Dougherty, B.L. Liu, and J.M. O'Farrell.

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

  • 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

  • High frequency flow/structural interaction in dense subsonic fluids [microform] / B.-L. Liu and J.M. O'Farrell.

    • Text
    • Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Implementation and validation of a wake model for low-speed forward flight [microform] : final technical report, October 1, 1986 to September 30, 1987 / Narayanan M. Komerath, Olivier A. Schreiber.

    • Text
    • Atlanta, Ga. : School of Aerospace Engineering, Georgia Institute of Technology ; [Hampton, Va. : National Aeronautics and Space Administration], Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Spurious frequencies as a result of numerical boundary treatments [microform] / Saul Abarbanel, David Gottlieb.

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

  • The acoustic characteristics of turbomachinery cavities [microform] / M.J. Lucas ... [et al.].

    • Text
    • [MSFC, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Prediction of vortex shedding from circular and noncircular bodies in subsonic flow [microform] / Michael R. Mendenhall and Daniel J. Lesieutre.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space 16
    • 1986

  • Vortex interaction with a leading-edge of finite thickness [microform] / by D. Sohn and D. Rockwell.

    • Text
    • Bethlehem, Penn. : Lehigh University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Numerical simulation of the flow about the F-18 HARV at high angle of attack [microform] / Scott M. Murman.

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

  • Impulsive start of a symmetric airfoil at high angle of attack [microform] / Joseph Katz, Steven Yon, Stuart E. Rogers.

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

  • Low speed aerodynamics of the X-38 CRV [microform] : final report, E16-N63 / Komerath, N.M. ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Development of a hybrid RANS/LES method for compressible mixing layer simulations [microform] / Nicholas J. Georgiadis, J. Iwan D. Alexander and Eli Reshotko.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22903

  • Secondary frequencies in the wake of a circular cylinder with vortex shedding [microform] / Saul S. Abarbanel ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67941

  • 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

  • A comparative study of some dynamic stall models [microform] / T.S. R. Reddy and K.R.V. Kaza.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92360

  • Navier-Stokes calculations for the vortex wake of a rotor in hover [microform] / C.H. Liu, J.L. Thomas, and C. Tung.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; St. Louis, Mo. : United States Army Aviation Systems Command, [1984]
    • 1984

  • Numerical simulation of vortex breakdown [microform] / Shi Xungang.

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

  • One-degree-of-freedom motion induced by modeled vortex shedding / L.A. Yates ... [and others].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS105809

  • One-degree-of-freedom motion induced by modeled vortex shedding [microform] / L.A. Yates ... [et al.].

    • 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/LPS105809

  • Simulation of self-induced unsteady motion in the near wake of a Joukowski airfoil [microform] / K.N. Ghia, G. A. Osswald, and U. Ghia.

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

  • An experimental study of airfoil-spoiler aerodynamics [microform] / Blair G. McLachlan and K. Karamcheti.

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

  • Experimental verification of buffet calculation procedure using unsteady PSP / Jayanta Panda.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67582

  • The transition from thick to thin plate wake physics : whither vortex shedding? / Man Mohan Rai.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, March 2016.
    • 2016-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68595

  • Assessment of JVX proprotor performance data in hover and airplane-mode flight conditions / C.W. Acree, Jr.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68686

  • Changes in flat plate wake characteristics obtained with decreasing plate thickness / Man Mohan Rai.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, July 2016.
    • 2016-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71758

  • Shed vortex structure and phase-averaged velocity statistics in symmetric/asymmetric turbulent flat plate wakes / Man Mohan Rai.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, June 2017.
    • 2017-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82367

  • Development of a hybrid RANS/LES method for compressible mixing layer simulations / Nicholas J. Georgiadis, J. Iwan D. Alexander and Eli Reshotko.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2001.
    • 2001-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22903

  • Intermittency and cessation of vortex shedding in the wake of a thin flat plate with a circular trailing edge / Man Mohan Rai.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, August 2018.
    • 2018-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo111056

  • Force evaluation in the lattice Boltzmann method involving curved geometry / Renwei Mei ... [and others].

    • Text
    • Hampton, Va. : ICASE, NASA Langley Research Center ; [Springfield, Va. :] : [For sale by the National Technical Information Service], [2002]
    • 2002
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60498

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta