archaeology
发表于 2025-3-25 07:24:29
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粘连
发表于 2025-3-25 08:11:00
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精密
发表于 2025-3-25 15:34:13
Conference proceedings 1998mputational modeling of partial differential equations pertinent primarily to aeronautical applications. The reader will find five survey articles on cartesian mesh methods, on numerical studies of turbulent boundary layers, on efficient computation of compressible flows, on the use of Riemann-solvers and on numerical procedures in complex flows.
Nerve-Block
发表于 2025-3-25 16:17:04
Lecture Notes in Physicshttp://image.papertrans.cn/s/image/868148.jpg
小卒
发表于 2025-3-25 22:56:41
https://doi.org/10.1007/BFb0106552calculus; fluid dynamics; modeling; numerical methods; partial differential equation; fluid- and aerodyna
壕沟
发表于 2025-3-26 00:57:33
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CYT
发表于 2025-3-26 05:32:47
Approximation of compressible flows by a reduced order model,D). The POD basis functions are used to filter, at each time step, the solution obtained from a finite-volume code. Three test cases are discussed: unsteady Euler flow about an oscillating airfoil, laminar vortex shedding from a NACA-0012 airfoil at incidence, and finally turbulent vortex shedding from a square cylinder.
尊重
发表于 2025-3-26 12:13:41
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Fatten
发表于 2025-3-26 12:38:39
A supersonic inverse wing design method and its application to Japanese SST, of . .=2.0. Several design constraints need to be satisfied. By means of the method, a wing has been designed which has desirable aerodynamic characteristics while using only a small amount of computation time.
Albinism
发表于 2025-3-26 19:42:54
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