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- W855550332 abstract "Mach number effects on pressure caused incipient separation of turbulent boundary layer in two dimensional supersonic corner flow" @default.
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- W855550332 date "1969-01-31" @default.
- W855550332 modified "2023-09-26" @default.
- W855550332 title "Incipient separation of a turbulent boundary layer at high Reynolds number in two- dimensional supersonic flow over a compression corner" @default.
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