Effects of the airfoil probes on the aerodynamic performance of a transonic compressor cascade
Author:
Funder
National Natural Science Foundation of China
National Major Science and Technology Projects of China
National Key Laboratory Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference37 articles.
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2. Parasitic loss due to leading edge instrumentation on a low-pressure turbine blade;Ng;J. Turbomach. Trans. ASME,2017
3. Investigation of the effects of airfoil-probes on the aerodynamic performance of an axial compressor;He;Chin. J. Aeronaut.,2012
4. Numerical analysis of an instrumented turbine blade cascade;Ubald;J. Turbomach.,2019
5. Effects of airfoil-probe tubes on the flow field of a compressor cascade;Ma;J. Therm. Sci.,2017
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