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Performance Enhancement of a Transonic Axial Compressor Stage with Gurney Flaps at Rotor Blade Trailing End

  • Coverage

    International

  • Type

    Non-Indexed

  • Published

  • Publisher

    Proceedings of Asian Congress on Gas Turbines, Indian Institute of Technology Bombay, Mumbai.

  • Cite As

    Mudassir Ahmed, M. R. and Nagpurwala, Q. H. (2016) Performance Enhancement of a Transonic Axial Compressor Stage with Gurney Flaps at Rotor Blade Trailing End, Proceedings of Asian Congress on Gas Turbines, Indian Institute of Technology Bombay, Mumbai.