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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2023
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Article
/
Tab 2
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Research Article
Effects of the Shock Wave Structure on the Tip Clearance Leakage Flow in Transonic Compressor Rotors
Table 2
Number of grid points.
Grid points
290,000
41
57
109
390,000
49
65
109
500,000
57
73
109
610,000
65
81
109
750,000
69
85
109