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  • B-1 AFT nacelle flow visualization study [microform] / James L. Gunter and Robert Celniker.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1975]
    • 1975

  • Ducted fan acoustic radiation including the effects of nonuniform mean flow and acoustic treatment [microform] / Walter Eversman, Indranil Danda Roy.

    • Text
    • Rolla, Mo. : Dept. of Mechanical and Aerospace Engineering and Engineering Mechanics, Univ. of Missouri-Rolla ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Computation of the transonic flow about a swept wing in the presence of an engine nacelle [microform] / D. Ross.

    • Text
    • [New York, N.Y.?] : Courant Mathematics and Computing Laboratory ; [Washington, D.C. : National Aeronautics and Space Administration] ; Springfield, VA : Available from National Technical Information Service, [1985]
    • 1985

  • Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS) [microform] : abstract / Mohamed E. Eleshaky and Oktay Baysal.

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

  • Fan noise prediction assessment [microform] / Paul H. Bent.

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

  • An analysis for high speed propeller-nacelle aerodynamic performance prediction [microform] / T. Alan Egolf ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988.
    • 1988

  • Finite difference time marching in the frequency domain [microform] : a parabolic formulation for aircraft acoustic nacelle design / Kenneth J. Baumeister and Kevin L. Kreider.

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

  • XV-15 structural-acoustic data [microform] / Karen H. Lyle.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Experimental and theoretical study of flow fields around ducted-nacelle models [microform] / Robert J. Mack.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Advanced turbofan duct liner concepts [microform] / Gerald W. Bielak and John W. Premo, Alan S. Hersh.

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

  • Short Haul Civil Tiltrotor study in MIDAS [microform] : auto vs manual nacelle procedures for commanded go-around / Adolph Atencio, Jr.; Carolyn Banda.

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

  • Some acoustic results from the Pratt and Whitney Advanced Ducted Propulsor [microform] : Fan 1 / James H. Dittmar and David M. Elliott, Lawrence A. Bock.

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

  • Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds [microform] / Robert J. Mack.

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

  • Performance optimization of a rotor alone Nacelle for acoustic fan testing [microform] / C.C. Cunningham, W.K. Thompson, and C.E. Hughes.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • Design and integration of a rotor alone nacelle for acoustic fan testing [microform] / Tony D. Shook ... [et al.].

    • 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/LPS26886

  • Advanced nacelle acoustic lining concepts development [microform] / G. Bielak ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60573

  • Interactive calculation procedures for mixed compression inlets [microform] / Eli Reshotko.

    • Text
    • Cleveland, Ohio : Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60916

  • Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport [microform] / Milton Lamb and William K. Abeyounis.

    • 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

  • An experimental investigation of propfan installations on an unsewpt supercritical wing at transonic Mach numbers [microform] / Glynn R. Bartlett.

    • Text
    • Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88314

  • Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development / Daniel L. Tweedt.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55838

  • Computational aerodynamic simulations of a 1215 ft/sec tip speed transonic fan system model for acoustic methods assessment and development / Daniel L. Tweedt.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55841

  • Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design / Kenneth J. Baumeister and Kevin L. Kreider.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, September 1996.
    • 1996-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68473

  • Experimental and theoretical study of flow fields around ducted-nacelle models / Robert J. Mack.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1998.
    • 1998-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83035

  • Performance optimization of a rotor alone Nacelle for acoustic fan testing / C.C. Cunningham, W.K. Thompson, and C.E. Hughes.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2000.
    • 2000-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo86221

  • Design and integration of a rotor alone nacelle for acoustic fan testing / Tony D. Shook [and five others].

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS26886

  • An over-the-rotor liner investigation with configurations enabled by additive manufacturing / Michael G. Jones.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2020.
    • 2020-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo151847

  • Pratt & Whitney/Boeing engine validation of noise reduction concepts : final report for NASA contract NAS3-97144. phase 2 / Larry A. Bock [and six others].

    • Text
    • East Hartford, Connecticut : United Technologies Corporation, Pratt & Whitney ; Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2014.
    • 2014-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53490

  • Methods for estimating drag polars of subsonic airplanes.

    • Text
    • [Lawrence? Kan.], [1971]
    • 1971
    • 1 Item
    FormatCall NumberItem Location
    Text TL574.D7R67Off-site

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