asghari shahrivar, anese
master student, Mech. Eng., Science and Research Branch, Islamic Azad University, Tehran, Iran.
[ 1 ] - Numerical Simulation Of the Componend Angles Effects On Adiabatic Film Cooling Effectiveness
Abstract Film Cooling Adiabatic Effectiveness on a Profile of a Gas Turbine blade that Using Holes with 45 Degree Combined Angles to the Flow Direction and Radial Along the Attack Edge as well as 25 Degree Angles to the Flow Direction and Surface Area of the Attack Edge Area and 35 degrees relative to the outlet hole suefaces along stagnation line, Under a specified blowing ratios, using the Re...
نویسندگان همکار