Abstract: A systematic and rational methodology for the calculation of an equilibrium state from an initial nonuniform flow field, is presented with particular emphasis on the underlying assumptions and ...

Abstract: The evolution of upstream propagating shock waves from the isolated transonic compressor designated NASA Rotor-35 is examined numerically. Results from the numerical simulations are compared with ...

Abstract: A numerical investigation of the unsteady aerodynamics of a fan stage comprised of a transonic rotor, swept fan exit guide vane (FEGV), and low-pressure compressor inlet guide vane (IGV) is ...

Abstract: The present study is concerned with the unsteady flow field on the blade outer air seal segments of high-work turbines; these segments are installed between the blade tip and outer casing and ...