Can I read Turbine Vane Endwall Cooling Analysis on EtoBox?

Turbine Vane Endwall Cooling Analysis by Badal Mishra is a document available to read on EtoBox.

What is Turbine Vane Endwall Cooling Analysis about?

This study investigates the effects of mid-passage gap with variable surface angles on the aerothermal and film cooling performances of turbine vane endwalls. Results show that using a 45° surface angle improves cooling effectiveness by suppressing secondary vortices, while a 135° angle significantly enlarges the coverage area on the pressure-side endwall. The optimal configuration combines a 135° upstream angle and a 45° downstream angle, resulting in a 43% increase in coverage area and a 37% increase in f

Author

Badal Mishra

Language

EN