commute
发表于 2025-3-28 17:54:51
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山顶可休息
发表于 2025-3-28 19:37:06
Extension, Validation and Application of the DA VII Transonic Airfoil Code with Passive Shock Controairfoil code to passive shock control (SC) by the incorporation of a SC law procedure for the prediction of the ventilation velocity and by the modification of the boundary conditions and of the algebraic eddy viscosity turbulence model for wall mass flow..Using the data base of Task 3 the extended
lethargy
发表于 2025-3-29 01:39:33
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闲荡
发表于 2025-3-29 04:41:25
Transonic Airfoil Flow Prediction with Shock Boundary Layer Interaction Control (SBLIC) by a Time-Acs code. With this code it was demonstrated that it can successfully be used below (steady flow) as well as above (unsteady flow) the buffet boundary. The code has been modified to account for shock control taking into account a porous surface close to the shock wave. Several control laws have been i
Conflagration
发表于 2025-3-29 08:15:50
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直觉好
发表于 2025-3-29 14:28:16
Introductiono study, numerically and experimentally, the effect of passive shock boundary layer interaction control (SBLIC) by ventilation on the design and off-design performance of primarily laminar-type airfoils and wings. The considerations leading to this research are outlined in what follows.
羞辱
发表于 2025-3-29 17:08:01
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放牧
发表于 2025-3-29 22:17:48
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Odyssey
发表于 2025-3-30 00:33:49
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Affluence
发表于 2025-3-30 07:29:59
https://doi.org/10.1007/978-3-658-27359-0nfigurations at steady and unsteady flow conditions. The main objective of the work was to extend existing methods to treat flows with shock control by modeling passive control through a perforated surface at the position of the shock and implementing the corresponding boundary conditions into the e