Allure 发表于 2025-3-26 22:25:17
http://reply.papertrans.cn/83/8232/823102/823102_31.png褪色 发表于 2025-3-27 04:01:42
http://reply.papertrans.cn/83/8232/823102/823102_32.pngGROSS 发表于 2025-3-27 05:56:03
Aerodynamic Design of Wing-Engine Configuration under Effect of Jet Plume,er-Stokes solver. The jet plume is considered in the analysis mode and the effect of the jet on/off is discussed. The inverse design method used here improves the L/D performance. Although the target M. is not achieved, the M. is also improved.otic-capsule 发表于 2025-3-27 11:20:08
http://reply.papertrans.cn/83/8232/823102/823102_34.pngCardiac-Output 发表于 2025-3-27 13:58:43
Inverse Blade Design Based on Permeable Wall Concept,ations. It is shown how the method can be combined with potential flow methods, Euler and Navier Stokes solvers. Each method is illustrated with examples. Advantages and problems are discussed and practical solutions to the existancy problem and mechanical constraints are proposed.占卜者 发表于 2025-3-27 21:44:35
0179-9614 lytical tool for both fundamental and practical fluid dynamics research. The analysis of flow fields is important in the sense that it improves the researcher‘s understanding of the flow features. CFD analysis also indirectly helps the design of new aircraft and/or spacecraft. However, design methodConcrete 发表于 2025-3-28 01:01:25
http://reply.papertrans.cn/83/8232/823102/823102_37.pnggait-cycle 发表于 2025-3-28 05:21:36
Subsonic Aerodynamic Design Via Optimization,ween the design and actual pressure distributions and/or minimizes induced drag is found iteratively using an optimization technique. Geometrical constrains and regularity conditions can be specified by means of penalty function concept and the requested values of lift and moment coefficients can be enforced using Lagrange multipliers technique.无所不知 发表于 2025-3-28 08:16:27
http://reply.papertrans.cn/83/8232/823102/823102_39.png我还要背着他 发表于 2025-3-28 10:35:08
Numerical Methods for Inverse Solution in Aerodynamic Design of Turbomachinery,-correction technique(DS-RC). The application of these methods and computer codes to turbine and compressor design has shown that the use of inverse solution techniques enables engineers to improve the design. A set of calculation examples and figures is also illustrated in the paper.