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  1. No Access

    Article

    Aerodynamic Performance of Multi-stage Axial Compressor Considering Cold-to-Hot Deformation Effect

    Predicting the exact performance of multi-stage compressors for an aircraft gas turbine is important in the design process and calculation of off-design characteristics. This study explores the quantitative ef...

    Sangjo Kim, Kuisoon Kim, Changmin Son in International Journal of Aeronautical and … (2018)

  2. No Access

    Article

    Adaptation Method for Overall and Local Performances of Gas Turbine Engine Model

    An adaptation method was proposed to improve the modeling accuracy of overall and local performances of gas turbine engine. The adaptation method was divided into two steps. First, the overall performance para...

    Sangjo Kim, Kuisoon Kim, Changmin Son in International Journal of Aeronautical and … (2018)