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Showing 1 to 4 of 4 for “"Unsteady Stator-rotor"”.

  1. Active Flow Control For Reduction of Unsteady Stator-Rotor Interaction In a Turbofan Simulator

    … trailing edge blowing control to reduce the unsteady stator-rotor interaction in a turbofan simulator. Two active flow control systems with different wake sensing approaches are successfully implemented on the engine simulator. The first flow control system utilizes Pitot probes as flow …

    vt Repository record for Active Flow Control For Reduction of Unsteady Stator-Rotor Interaction In a Turbofan Simulator (opens in a new tab)

  2. Reduction of Unsteady Stator-Rotor Interaction by Trailing Edge Blowing Using MEMS Based Microvalves

    … to variations in flow parameters and reduce the unsteady stator-rotor interaction at all engine operating conditions. The fan rotor of a 1/14 scale turbofan propulsion simulator is subjected to spatially periodic, circumferential inlet flow distortions. The distortions are generated by four …

    vt Repository record for Reduction of Unsteady Stator-Rotor Interaction by Trailing Edge Blowing Using MEMS Based Microvalves (opens in a new tab)

  3. Effects of Inlet Guide Vane Flow Control on Forced Response of a Transonic Fan

    … functions generated by an upstream row of stators or inlet guide vanes. Resonant response to engine order excitation at certain rotor speeds is especially damaging. Studies have shown that flow control by trailing edge blowing (TEB) can reduce stator wake strength and the amplitude of the …

    vt Repository record for Effects of Inlet Guide Vane Flow Control on Forced Response of a Transonic Fan (opens in a new tab)

  4. Investigation of Inlet Guide Vane Wakes in a F109 Turbofan Engine with and without Flow Control

    … in a F109 turbofan engine to investigate the unsteady wake profiles of an Inlet Guide Vane (IGV) at a typical spacing to the downstream fan at subsonic and transonic relative blade velocities. The sharp trailing-edge vanes were designed to produce a wake profile consistent with modern IGV. …

    vt Repository record for Investigation of Inlet Guide Vane Wakes in a F109 Turbofan Engine with and without Flow Control (opens in a new tab)