Browsing by Subject "Gas Turbine Heat Transfer"
Now showing items 1-3 of 3
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(2022-06-07)Serpentine, multi-pass cooling passages are used for cooling advanced gas turbine blades. In open literature, most internal cooling studies use a fixed cross-sectional area for multi-pass channels. Studies that use varying ...
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(2009-06-02)The present work has been an experimental investigation to evaluate the applicability of gas turbine cooling technology. With the temperature of the mainstream gas entering the turbine elevated above the melting temperature ...
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(2018-07-27)The flow around a gas turbine blade is inherently three-dimensional and based on the Re-number and the blade geometry, it may be laminar, transitional or turbulent. The blade surfaces are subject to periodic unsteady wakes ...