Improving turbine endwall cooling uniformity by controlling near-wall secondary flows

In this paper, we propose a design philosophy for cooling high-pressure nozzle guide vane endwalls, which exploits the momentum of cooling jets to control vane secondary flows thereby improving endwall cooling uniformity. The impact of coolant-to-mainstream pressure ratio, hole inclination angle, ho...

সম্পূর্ণ বিবরণ

গ্রন্থ-পঞ্জীর বিবরন
প্রধান লেখক: Thomas, M, Povey, T
বিন্যাস: Journal article
প্রকাশিত: SAGE Publications 2016