Experimental and numerical simulations were conducted on turbine blade to figure out influences of three typical factors(vane curvature
blowing ratio and hole arrangement)on superposition prediction of film cooling efficiency. Results show that because of the convex blade surface on the suction side
jet is easy to be blown off and the computational error of superposition of film cooling efficiency is about 5%. On the pressure side
jet is easy to be pressed onto the wall and the prediction becomes inaccurate
hence the superposition calculation result is about 13% higher than experimental value. Another significant influence results from hole arrangement
the superposition prediction on staggered hole arrangement is nearly the same as the measured value
while it is much higher for in-line arrangement. Blowing ratio also has an obvious influence on the accuracy of superposition prediction for film cooling holes on both pressure side and suction side. At low blowing ratio
results obtained by Sellers method agree well with the experimental ones
while as blowing ratio increases
the accuracy of superposition prediction is decreased. At last
modification of Sellers method is suggested to improve the prediction accuracy.
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references
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