標(biāo)題: Titlebook: Recent Development of Aerodynamic Design Methodologies; Inverse Design and O Kozo Fujii,George S. Dulikravich Book 1999 Springer Fachmedien [打印本頁] 作者: APL 時間: 2025-3-21 18:22
書目名稱Recent Development of Aerodynamic Design Methodologies影響因子(影響力)
書目名稱Recent Development of Aerodynamic Design Methodologies影響因子(影響力)學(xué)科排名
書目名稱Recent Development of Aerodynamic Design Methodologies網(wǎng)絡(luò)公開度
書目名稱Recent Development of Aerodynamic Design Methodologies網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Recent Development of Aerodynamic Design Methodologies被引頻次
書目名稱Recent Development of Aerodynamic Design Methodologies被引頻次學(xué)科排名
書目名稱Recent Development of Aerodynamic Design Methodologies年度引用
書目名稱Recent Development of Aerodynamic Design Methodologies年度引用學(xué)科排名
書目名稱Recent Development of Aerodynamic Design Methodologies讀者反饋
書目名稱Recent Development of Aerodynamic Design Methodologies讀者反饋學(xué)科排名
作者: 光亮 時間: 2025-3-21 21:39 作者: LAY 時間: 2025-3-22 03:24
Recent Development of Aerodynamic Design Methodologies978-3-322-89952-1Series ISSN 0179-9614 作者: Munificent 時間: 2025-3-22 07:13
Notes on Numerical Fluid Mechanicshttp://image.papertrans.cn/r/image/823102.jpg作者: 詞根詞綴法 時間: 2025-3-22 09:12 作者: slipped-disk 時間: 2025-3-22 16:34 作者: Employee 時間: 2025-3-22 19:01
Using Existing Flow-Field Analysis Codes for Inverse Design of Three-Dimentional Aerodynamic Shapesdesign process is found to be similar for both non-lifting and lifting aerodynamic shapes with the Navier-Stokes flow solver typically requiring minimum number of design iterations. Suggestions for further research and improvements are made.作者: 輪流 時間: 2025-3-22 21:32
An Inverse Design Method for Wings Using Integral Equations and Its Recent Progress,quations which govern the flowfield. The first inverse problem is for transonic wing design. The second one is for supersonic and the third one is for design of multiple wing systems. Emphasis is put on the discussion of the formulation. Works on wing design using the method with the first inverse p作者: 發(fā)微光 時間: 2025-3-23 04:34
Book 1999e for such methods to be used practically. There is strong evidence of a growing interest in the development and use of aerodynamic inverse design and optimization techniques. This is true, not only for aerospace industries, but also for any industries requiring fluid dynamic design. This clearly sh作者: 為寵愛 時間: 2025-3-23 08:08 作者: 碌碌之人 時間: 2025-3-23 10:12
Carlo Poloni, on the other hand, they are also a means to promote European integration. It is often assumed that EU officials consider CSOs to be vehicles for selling the EU to its citizens or to be cheerleaders for European integration (Cullen 2010). A closer analysis of this presumed function shows that such 作者: diskitis 時間: 2025-3-23 15:31 作者: 煩擾 時間: 2025-3-23 19:48 作者: braggadocio 時間: 2025-3-24 01:00 作者: 不足的東西 時間: 2025-3-24 03:06
George S. Dulikravich,Daniel P. Bakeruropean Commission decided to create a single European market with unrestricted social mobility between member states. The process of German unification, which commenced in the autumn of 1989 and resulted in East Germany joining the West on 3 October 1990, had always been linked to an emphatic commi作者: Cholagogue 時間: 2025-3-24 08:16
Naixing Chen the making since 1945.. British people and the British mass media (the BBC included) still think of themselves as being separate from the rest of Europe. They refer in conversation, as much as in news broadcasts, to ‘Britain and Europe’, to ‘going across to Europe’, to ‘the continent of Europe’. Ou作者: 叫喊 時間: 2025-3-24 13:55
R. A. Van den Braembusschepart remain unclear. We can be sure that West German policy-makers and business leaders will shift their attentions from the challenges posed by 1992 to those offered in the East as the difficulties involved in unifying two rather different sets of economic structures unfold. To some extent this has作者: unstable-angina 時間: 2025-3-24 17:07
Kisa Matsushima,Susumu Takanashi the making since 1945.. British people and the British mass media (the BBC included) still think of themselves as being separate from the rest of Europe. They refer in conversation, as much as in news broadcasts, to ‘Britain and Europe’, to ‘going across to Europe’, to ‘the continent of Europe’. Ou作者: 使困惑 時間: 2025-3-24 21:21
Takeshi Kaidenot least by the Northern victory in 1865. Slavery and Southern rebellion seemed to verify that danger could easily proceed from the periphery, and the ratification of the Fourteenth Amendment subsequently protected constitutionally guaranteed rights from state abuse. The twentieth century, especiall作者: 厭倦嗎你 時間: 2025-3-25 01:01 作者: aerobic 時間: 2025-3-25 05:38 作者: STRIA 時間: 2025-3-25 08:54 作者: Left-Atrium 時間: 2025-3-25 14:47
Application of Transonic Inverse Method to the Development of Aerospace Products,en the specified and computed pressure distribution, starting from a baseline geometry..This paper shows two applicated examples of this inverse problem. One is for swept wing of typical civil transport. The other is for non-planar wing of H-II Orbiting Plane(HOPE) tipfin configuration.作者: GET 時間: 2025-3-25 18:44
Multi Objective Aerodynamic Optimisation by Means of Robust and Efficient Genetic Algorithm,thodologies the operators considered at present the most promising one are described. A simple mathematical test is used for preliminary algorithmic perfomance while in more applicative cases the pressure reconstruction problem of two conflicting aerodynamic profiles is used as benchmark. A full pot作者: Gum-Disease 時間: 2025-3-25 22:13 作者: EXULT 時間: 2025-3-26 03:24
Subsonic Aerodynamic Design Via Optimization,of attack. Effects of flaps deflection can be incorporated and the induced drag can be minimized. A higher order panel method is applied to perform flow analysis. Flaps deflection is simulated by modifying a Neumann boundary conditions. In the design case the geometry which minimizes differences bet作者: 染色體 時間: 2025-3-26 04:38 作者: exceptional 時間: 2025-3-26 10:10 作者: 是他笨 時間: 2025-3-26 14:19
Numerical Methods for Inverse Solution in Aerodynamic Design of Turbomachinery,function(SF) method of two different kinds of stream surfaces, which are usually assumed for the design in turbomachinery, stream-function-coordinate(SFC) method for two-dimensional and three-dimensional flows, potential function(PF) method and the method based on the direct solution with a residual作者: 群居男女 時間: 2025-3-26 20:28
Inverse Blade Design Based on Permeable Wall Concept,ed how the permeable wall concept can be used to define the blade modifications required to obtain the target performances with a small number of iterations. It is shown how the method can be combined with potential flow methods, Euler and Navier Stokes solvers. Each method is illustrated with examp作者: Allure 時間: 2025-3-26 22:25 作者: 褪色 時間: 2025-3-27 04:01 作者: GROSS 時間: 2025-3-27 05:56
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.作者: otic-capsule 時間: 2025-3-27 11:20 作者: Cardiac-Output 時間: 2025-3-27 13:58
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.作者: 占卜者 時間: 2025-3-27 21:44
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 method作者: Concrete 時間: 2025-3-28 01:01 作者: gait-cycle 時間: 2025-3-28 05:21
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.作者: 無所不知 時間: 2025-3-28 08:16 作者: 我還要背著他 時間: 2025-3-28 10:35
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.作者: muster 時間: 2025-3-28 18:27 作者: Glucose 時間: 2025-3-28 21:09 作者: 衰弱的心 時間: 2025-3-29 02:04
