Research Catalog

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  • A review of turbomachinery blade-row interaction research [microform] / Todd E. Smith.

    • Text
    • Cleveland, Ohio : Lewis Research Center, National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1988]
    • 1988

  • Small-amplitude disturbances in turbomachine flows with swirl [microform] / David W. Wundrow.

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

  • Multigrid calculation of three-dimensional turbomachinery flows [microform] / David A. Caughey.

    • Text
    • Ithaca, New York : Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University ; [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Development of a turbomachinery design optimization procedure using a multiple-parameter nonlinear perturbation method [microform] / Stephen S. Stahara.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1984.
    • 1984

  • A study of internal and distributed damping for vibrating turbomachiner blades [microform] / Arthur W. Leissa.

    • Text
    • Columbus, OH : Ohio State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • NASA Lewis Research Center Workshop on Forced Response in Turbomachinery [microform] : proceedings of a conference ... held at the NASA Lewis Research Center, Cleveland, Ohio, August, 11, 1993.

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

  • Sensitivity analysis for aeroacoustic and aeroelastic design of turbomachinery blades [microform] : final technical report / Christopher B. Lorence and Kenneth C. Hall.

    • Text
    • Durham, NC : Dept. of Mechanical Engineering and Materials Science, School of Engineering, Duke University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • TADS, a CFD-based turbomachinery and analysis design system with GUI [microform] / D.A. Topp, R.A. Myers, and R.A. Delaney.

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

  • A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows [microform] / Matthew D. Montgomery and Joseph M. Verdon.

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

  • Design, fabrication, and testing of a high-speed, over-running clutch for rotorcraft [microform] / Frank Fitz and Craig Gadd.

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

  • Time-of-flight tip-clearance measurements [microform] / H.S. Dhadwal, A.P. Kurkov and D.C. Janetzke.

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

  • Application of TURBO-AE to flutter prediction [microform] : aeroelastic code development / Daniel Hoyniak, Todd A. Simons ; [prepared under contract NAS3-27725 task 6 EDR-19540].

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

  • 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

  • Gust response analysis of a turbine cascade [microform] / R.S.R. Gorla ... [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/LPS26732

  • Calculation of transonic flow in a linear cascade [microform] / Leo F. Donovan.

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

  • Programs for calculating quasi-three-dimensional flow in a turbomachine blade row [microform] / Theodore Katsanis.

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

  • 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

  • Improved finite-difference vibration analysis of pretwisted, tapered beams [microform] / K.B. Subrahmanyam and K.R.V. Kaza.

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

  • Turbine blade thermal fatigue testing Pratt and Whitney aircraft hollow core blades [microform] / by Jeff Ingram and Loren Gross.

    • Text
    • [Marshall Space Flight Center, Ala.?] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1985]
    • 1985

  • Probabilistic structural analysis methods of hot engine structures [electronic resource] / C. C. Chamis and D. A. Hopkins.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108448

  • Probabilistic structural analysis methods of hot engine structures [microform] / C. C. Chamis and D. A. Hopkins.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108448

  • The influence of gyroscopic forces on the dynamic behavior and flutter of rotating blades / F. Sisto and A.T. Chang.

    • Text
    • Hoboken, N.J. : Department of Mechanical Engineering, Stevens Institute of Technology ; Cleveland, Ohio : Lewis Research Center, National Aeronautics and Space Administration, 1983.
    • 1983
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo46856

  • The influence of gyroscopic forces on the dynamic behavior and flutter of rotating blades / F. Sisto and A.T. Chang.

    • Text
    • Hoboken, N.J. : Department of Mechanical Engineering, Stevens Institute of Technology ; Cleveland, Ohio : Lewis Research Center, National Aeronautics and Space Administration, 1983.
    • 1983

  • Comparison of computational aeroacoustics prediction of acoustic transmission through a 3D stator with experiment / Ray Hixon [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2014.
    • 2014-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54282

  • Gust response analysis of a turbine cascade / R.S.R. Gorla [and three others].

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS26732

  • 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

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