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发表于 2025-3-21 23:20:23
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发表于 2025-3-22 03:00:15
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发表于 2025-3-22 07:48:19
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发表于 2025-3-22 11:19:47
Snehasikta Swarnakar,Amartya Mishra,Susri Ray Chaudhuri (Guha)s as Re. → ∞, or has involved approximate double-layered models for supersonic flow with insufficient consideration of the basic flow structure in the shear-disturbance sublayer . Consequently, there is a need for a more general theory at ordinary practical Reynolds numbers, applic
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发表于 2025-3-22 14:39:39
Mange Ram Yadav,Prashant Revan Murumkar,Vishal Prakash Zambre the interaction between viscous and inviscid regions and the calculation of pressure, velocity and temperature characteristics as a function of geometry, angle of attack and Mach number. Rather more than half the papers were concerned with two-dimensional configurations and the remainder with wings
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发表于 2025-3-22 18:39:11
Rajeshwar P. Verma involving the interaction between viscous and inviscid regions and the calculation of pressure, velocity and temperature characteristics as a function of geometry, angle of attack and Mach number. Rather more than half the papers were concerned with two-dimensional configurations and the remainder with wings978-3-662-09016-9978-3-662-09014-5
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前兆
发表于 2025-3-23 04:26:50
Mina M. Benjamin,Raouf A. Khalilfield have also been successful provided separation was not present . Recently an asymmetric trailing-edge flow with a small separated zone was successfully predicted using the Navier—Stokes equations . The ability to calculate trailing-edge flows with large separated zones remains to
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发表于 2025-3-23 08:55:57
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