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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
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Fig 29
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Research Article
Effects of the Shock Wave Structure on the Tip Clearance Leakage Flow in Transonic Compressor Rotors
Figure 29
Contour of entropy at the tip clearances at 10%, 50%, and 90% chords.
(a)
Rotor37
(b)
RotorSD