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  • Low noise research fan stage design [microform] / David E. Hobbs ... [et al.].

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

  • Coupled 2-dimensional cascade theory for noise and unsteady aerodynamics of blade row interaction in turbofans. Volume 1, Theory development and parametric studies [microform] / Donald B. Hanson.

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

  • Computational fluid dynamics study of the variable-pitch split-blade fan concept [microform] / C.E. Kepler, A.R. Elmquist and R.L. Davis.

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

  • Computation of noise radiation from turbofans [microform] : a parametric study / M. Nallasamy.

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

  • Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors [microform] : user's manual / James F. Schmidt.

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

  • Energy efficient engine component development & integration program [microform] : semiannual report no. 7, April 1, 1981 - September 30, 1981 / General Electric project manager, R.W. Bucy.

    • Text
    • Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, Advanced Engineering and Technology Programs Dept. ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1981]
    • 1981

  • Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows [microform] / J.G. Williams and W.G. Steenken, A.J. Yuhas.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Azimuthal patterns of the radiated sound field from a turbofan model [microform] / R.H. Thomas ... [et al.].

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

  • Advanced low-noise research fan stage design [microform] / Robert Neubert ... [et al.] ; prepared under contract NAS3-26618.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Lewis Research Center ; Available from Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • Quiet high-speed fan [microform] / Lysbeth Lieber, Russ Repp, and Donald S. Weir.

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

  • Energy efficient engine low pressure subsystem flow analysis [microform] / Edward J. Hall ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, [distributor, 1998]
    • 1998

  • Boeing 18-inch fan rig broadband noise test [microform] / Ulrich Ganz ... [et al.].

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

  • Design of a low speed fan stage for noise suppression [microform] / W.N. Dalton, D.B. Elliot, and K.L. Nickols.

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

  • Acoustic scattering by three-dimensional stators and rotors using the SOURCE3D code [microform] / Harold D. Meyer.

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

  • Static performance of six innovative thrust reverser concepts for subsonic transport applications [microform] : summary of the NASA Langley Innovative Thrust Reverser Test Program / Scott C. Asbury and Jeffrey A. Yetter.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22791

  • Ultra-efficient engine diameter study [microform] / David L. Daggett, Stephen T. Brown, and Ron T. Kawai.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55129

  • Turbofan noise propagation and radiation at high frequencies [microform] / Walter Eversman.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55130

  • Vibration and flutter of mistuned bladed-disk assemblies [microform] / Krishna Rao V. Kaza and Robert E. Kielb.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / Richard F. Bozak, Christopher E. Hughes, James Buckley.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
    • 2013-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49564

  • Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program / Scott C. Asbury and Jeffrey A. Yetter.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2000.
    • 2000-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22791

  • Flutter analysis of a transonic fan / R. Srivastava [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2002.
    • 2002-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS42474

  • Quiet High Speed Fan II (QHSF II) : final report / Karen Kontos, Don Weir, and Dave Ross.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32517

  • Performance and weight estimates for an advanced open rotor engine / Eric S. Hendricks and Michael T. Tong.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo33031

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