Experimental Investigation on Effect of Cross-Flow Reynolds Number on Film Cooling Effectiveness
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
2. AECC Commercial Aircraft Engine Co., Ltd, 200241 Shanghai, People’s Republic of China
Funder
National Natural Science Foundation of China
National Key Laboratory of Aerodynamic Design and Research
AECC union Foundation
Innovation Foundation for Doctor Dissertation of Northwestern Polytechnical University
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference26 articles.
1. Effect of Internal Coolant Crossflow on the Effectiveness of Shaped Film-Cooling Holes
2. In-hole and mainflow velocity measurements of low-momentum jets in crossflow emanating from short holes
3. The Effect of Internal Crossflow on the Adiabatic Effectiveness of Compound Angle Film Cooling Holes
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