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  • Modeling improvements and users manual for axial-flow turbine off-design computer code AXOD [microform] / Arthur J. Glassman.

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

  • Enhanced capabilities and updated users manual for axial-flow turbine preliminary sizing code TURBAN [microform] / Arthur J. Glassman.

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

  • Unsteady flows in a single-stage transonic axial-flow fan stator row [microform] / Michael D. Hathaway.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [St. Louis, MO] : U.S. Army Aviation Systems Command ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • Three dimensional viscous flow field in an axial flow turbine nozzle passage [microform] / D. Ristiʹc and B. Lakshminarayana.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines [microform] / A.A. Ameri, E. Steinthorsson, David L. Rigby.

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

  • The three dimensional flow field at the exit of an axial-flow turbine rotor [microform] / B. Lakshminarayana, D. Ristic, and S. Chu.

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

  • Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines / A.A. Ameri, E. Steinthorsson, David L. Rigby.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1998]
    • 1998
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30851

  • Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating / Vikram Shyam, Ali Ameri.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo31866

  • A guide to axial-flow turbine off-design computer program AXOD2 / Shu-cheng S. Chen.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2014.
    • 2014-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54360

  • Understanding and mitigating tip leakage and endwall losses in high pressure ratio cores / Jesse Christophel.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2015.
    • 2015-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo64459

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