Research Catalog

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

Selected filters.Clear Filters

  • Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight [microform] : interim technical report under NASA-Ames Research grant no. NAG-2-797 (August 1, 1992 - December 21, 1993) / G.H. Gaonkar, S. Subramanian, Srinivas Chunduru.

    • Text
    • Boca Raton, FL : Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering ; [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

  • Effect of acoustic excitation on stalled flows over an airfoil [microform] / K.B.M.Q. Zama.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • 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

  • 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

  • Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight [microform] : final technical report under NASA-Ames cooperative agreement no. NCC 2-361 (August 1, 1985 - July 31, 1987) / by G. Gaonkar.

    • Text
    • Boca Raton, FL : Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Flight determination of the aerodynamic stability and control characteristics of the NASA SGS 1-36 sailplane in the conventional and deep stall angles-of-attack of between -5 and 75 degrees [microform] / by Faramarz A. Mahdavi, Dral R. Sandlin.

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University, Aeronautical Engineering Dept. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Control of unsteady separated flow associated with the dynamic stall of airfoils [microform] : final report, 95-09 / M.C. Wilder.

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

  • A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region [microform] / Edward C. Polhamus.

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

  • The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data [microform] / C.M. Tan and L.W. Carr.

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

  • Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight [microform] : final technical report under NASA-Ames research grant no. NAG 2-797 / G.H. Gaonkar, S. Subramanian.

    • Text
    • Boca Raton, FL : Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Cellular structures in the flow over the flap of a two-element wing [microform] / Steven A. Yon and Joseph Katz.

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

  • 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

  • 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

  • Airfoil dynamic stall and rotorcraft maneuverability [microform] / William G. Bousman.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23428

  • Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane [microform] / H. Paul Stough III, Daniel J. DiCarlo, and James M. Patton, 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, 1985.
    • 1985

  • Some observations on transitory stall in conical diffusers [microform] / K.B.M.Q. Zaman and M.D. Dahl.

    • Text
    • Cleveland, Ohio : Lewis Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58502

  • Analysis of fully stalled compressor [microform] / Wojciech Rostafinski.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data [microform] / Robert Alan Hess.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85279

  • 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

  • An automated stall-speed warning system [microform] / Douglass O. Wilner and Glenn A. Bever.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • Performance degradation of a typical twin engine commuter type aircraft in measured natural icing conditions [microform] / Richard J. Ranaudo ... [et al.].

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS101204

  • Synthesized airfoil data method for predicttion of dynamic stall and unsteady airloads [microform] / Santu T. Gangwani.

    • 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/LPS104922

  • Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove / Trong T. Bui.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, January 2014.
    • 2014-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50966

  • Dynamic wind-tunnel testing of a sub-scale iced S-3B Viking / Sam Lee, Billy Barnhart, Thomas P. Ratvasky.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51477

  • Investigation of active flow control to improve aerodynamic performance of oscillating wings / Robert P. Narducci [and five others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2014.
    • 2014-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52595

  • Dynamic stall suppression using combustion-powered actuation (COMPACT) / Claude G. Matalanis [and nine others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2016.
    • 2016-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82480

  • Airfoil dynamic stall and rotorcraft maneuverability / William G. Bousman.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, July 2000.
    • 2000-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS23428

  • Analysis of an unswept propfan blade with a semiempirical dynamic stall model / T.S.R. Reddy, K.R.V. Kaza.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, January 1989.
    • 1989-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173227

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