-
1
Linearized unsteady aerodynamic analysis of the acoustic response to wake/blade-row interaction
[Cleveland, Ohio] : Hanover, Md. :; [Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2001Format: Government Document Book
//IF NOT LOGGED IN - FORCE LOGIN ?>
//ELSE THEY ARE LOGGED IN PROCEED WITH THE OPEN URL CODE:?> -
2
Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1996Format: Government Document Book
//IF NOT LOGGED IN - FORCE LOGIN ?>
//ELSE THEY ARE LOGGED IN PROCEED WITH THE OPEN URL CODE:?> -
3
Coupling of low speed fan stator vane unsteady pressures to duct modes : measured versus predicted
[Cleveland, Ohio] : Springfield, VA : National Aeronautics and Space Administration, Glenn Research Center ; National Technical Information Service, distributor, 1999Format: Government Document Book
//IF NOT LOGGED IN - FORCE LOGIN ?>
//ELSE THEY ARE LOGGED IN PROCEED WITH THE OPEN URL CODE:?> -
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], 1999Format: Government Document Book
//IF NOT LOGGED IN - FORCE LOGIN ?>
//ELSE THEY ARE LOGGED IN PROCEED WITH THE OPEN URL CODE:?> -
5
Computation of rotor-stator interaction using Navier-Stokes equations : final report
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], 1995Format: Government Document Book
//IF NOT LOGGED IN - FORCE LOGIN ?>
//ELSE THEY ARE LOGGED IN PROCEED WITH THE OPEN URL CODE:?>