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  1. 1

    Linearized unsteady aerodynamic analysis of the acoustic response to wake/blade-row interaction by Verdon, Joseph M.

    [Cleveland, Ohio] : Hanover, Md. :; [Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2001
    Format: Government Document Book


  2. 2

    Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine by Dorney, Daniel J.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


  3. 3

    Coupling of low speed fan stator vane unsteady pressures to duct modes : measured versus predicted by Sutliff, Daniel L.

    [Cleveland, Ohio] : Springfield, VA : National Aeronautics and Space Administration, Glenn Research Center ; National Technical Information Service, distributor, 1999
    Format: Government Document Book


  4. 4

    Blade heat transfer measurements and predictions in a transonic turbine cascade

    [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


  5. 5

    Computation of rotor-stator interaction using Navier-Stokes equations : final report by Whitfield, David L.

    Mississippi State, Miss. : [Washington, D.C.] : [Springfield, Va.] : CFD Lab, NSF Engineering Research Center for Computational Field Simulation, Mississippi State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book