The effect of gas compressibility on the effective flow area was studied by theory and experiment. The regression analysis method was used to fit the experimental data
and compared the degree of the coincidence between different theoretical models and experimental data. Results showed that the pressure of gas compressibility can be neglected when the gas pressure ratio was less than 1.081. When the pressure ratio was greater than 1.081
the fitting curve of the compressible gas theory model was consistent with the experimental data
and the value of effective flow area was stable at different pressure ratios. Fitting curves of the incompressible flow theory model deviated from the experimental data. The value of the effective flow area changed with different pressure ratios.
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Related Author
FU Peng
ZHAO Guochao
WANG Hui
ZHANG Changshuai
LI Huacong
SU Zhishan
张堃元
马元
Related Institution
School of Mechanical Engineering,Liaoning Technical University
南京航空航天大学 能源与动力学院
中国航天科技集团有限公司 西安航天动力研究所
Department of Scientific Research Project, China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics