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Showing 1 to 20 of 52 for “"Rotating Stall"”.

  1. Distributed nonlinear stability analysis of rotating stall

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.

    mit Repository record for Distributed nonlinear stability analysis of rotating stall (opens in a new tab)

  2. Active control rotating stall with inlet distortion

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.

    mit Repository record for Active control rotating stall with inlet distortion (opens in a new tab)

  3. Nonlinear active control of rotating stall and surge

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.

    mit Repository record for Nonlinear active control of rotating stall and surge (opens in a new tab)

  4. Active control of rotating stall in axial compressors

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992.

    mit Repository record for Active control of rotating stall in axial compressors (opens in a new tab)

  5. Evaluation of rotating stall warning schemes for axial compressors

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992.

    mit Repository record for Evaluation of rotating stall warning schemes for axial compressors (opens in a new tab)

  6. Computational study of rotating stall in high-speed compressor

    Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.

    mit Repository record for Computational study of rotating stall in high-speed compressor (opens in a new tab)

  7. An experimental investigation of compressor performance in rotating stall

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1982.

    mit Repository record for An experimental investigation of compressor performance in rotating stall (opens in a new tab)

  8. Actuation for rotating stall control of high speed axial compressors

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.

    mit Repository record for Actuation for rotating stall control of high speed axial compressors (opens in a new tab)

  9. Time resolved measurements of rotating stall in axial flow compressors

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.

    mit Repository record for Time resolved measurements of rotating stall in axial flow compressors (opens in a new tab)

  10. Blade passage flow structure effects on axial compressor rotating stall inception

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.

    mit Repository record for Blade passage flow structure effects on axial compressor rotating stall inception (opens in a new tab)

  11. Active control of rotating stall in a three-stage axial compressor

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1993.

    mit Repository record for Active control of rotating stall in a three-stage axial compressor (opens in a new tab)

  12. Design of a jet actuator for active control of rotating stall

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.

    mit Repository record for Design of a jet actuator for active control of rotating stall (opens in a new tab)

  13. A study of the rotating-stall inception in high-speed compressors

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.

    mit Repository record for A study of the rotating-stall inception in high-speed compressors (opens in a new tab)

  14. Robust control of a surge and rotating stall in an axial compressor

    This thesis presents an investigation of the stability of axial compression systems when external disturbances are introduced. Aerodynamic stability is considered from a nonlinear perspective. From this perspective, the goal is to enhance the ability of compressor systems to remain stable in the …

    mit Repository record for Robust control of a surge and rotating stall in an axial compressor (opens in a new tab)

  15. A computational model for rotating stall and inlet distortions in multistage compressors

    … the non-linear aspects of short wavelength stall inception, part span stall cells, and compressor response to three-dimensional inlet distortions. The computed results demonstrated the first-of-a-kind capability for simulating short wavelength stall inception in multistage compressors. The …

    mit Repository record for A computational model for rotating stall and inlet distortions in multistage compressors (opens in a new tab)

  16. Experimental evaluation of asymmetric bleed actuation for rotating stall and surge control

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.

    mit Repository record for Experimental evaluation of asymmetric bleed actuation for rotating stall and surge control (opens in a new tab)

  17. Dynamic control of rotating stall in axial flow compressors using aeromechanical feedback

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.

    mit Repository record for Dynamic control of rotating stall in axial flow compressors using aeromechanical feedback (opens in a new tab)

  18. A two-dimensional model to predict rotating stall in axial-flow compressors

    … part of this ongoing effort, a model to simulate rotating stall inception and development in axial-flow compressor stages was constructed. This model was applied to an isolated rotor build to investigate the sensitivity of the predicted stall behavior to the shape of the high-incidence portions of …

    vt Repository record for A two-dimensional model to predict rotating stall in axial-flow compressors (opens in a new tab)

  19. Time-resolved measurements of a transonic compressor during surge and rotating stall

    … (about 20:1), good efficiency and sufficient stall margin. The rotor was tested without the presence of a stator (or any of the following seven stages) at the NASA Lewis single-stage, high-speed, core-compressor test-rig. The measurements were obtained with a single circumferential, …

    vt Repository record for Time-resolved measurements of a transonic compressor during surge and rotating stall (opens in a new tab)

  20. Modeling and control of rotating stall in high speed multi-stage axial compressors

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.

    mit Repository record for Modeling and control of rotating stall in high speed multi-stage axial compressors (opens in a new tab)

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