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[Mathimatics-Numerical algorithmscfdbooksoftware

Description: CFD BOOK Principles of Computational Fluid Dynamics的源代码-Principles of Computational Fluid Dynamics CODE
Platform: | Size: 131072 | Author: yanhongliang | Hits:

[Algorithmcebeci

Description: cebeci随书CFD程序 Fortran格式-cebeci with the CFD program Fortran format of the book
Platform: | Size: 6594560 | Author: zhou | Hits:

[OtherNumerical_Heat_Transfer

Description: CFD的一本实用书籍,里面介绍了CFD的一些基础,主要讲解有限体积法。-An useful book for CFD, some fundamental knowledge and elaborate introduction of FVM included.
Platform: | Size: 10144768 | Author: 枫叶 | Hits:

[OtherVersteeg

Description: a very good CFD book
Platform: | Size: 3338240 | Author: ejav | Hits:

[Industry researchMaTeyou-CFD

Description: 马铁犹-计算流体动力学,一本介绍CFD很好的书,希望大家有用-Ma Teyou-CFD, hope the book can help you.
Platform: | Size: 9294848 | Author: wds | Hits:

[AlgorithmJ-D-Anderson-CFD-Introduction

Description: 飞机气动计算流体力学分析的经典之作,值得学习的好书-a excellent book about aerodyanmics introduction
Platform: | Size: 6235136 | Author: 刘经纬 | Hits:

[matlabwesseling

Description: Matlab sources on CFD book by P.Wesseling
Platform: | Size: 43008 | Author: Includer | Hits:

[Other2D_LRe_ke

Description: 低雷诺k-epsilon 湍流模型方程,流体力学软件COMSOL 3.5的一个例子-This implemented Low-Re k-epsilon Comsol model is based on the Launder-Sharma damping functions as described in Wilcox s Turbulence modeling for CFD book. Model implementation was in 2D under steady state situation but it can be extended to 3D with relative ease.
Platform: | Size: 2642944 | Author: 高希 | Hits:

[Software Engineeringadvanced-cfd-book

Description: 超详细的高等计算流体力学讲义,零基础的飞跃提高,高清文字版,你懂的-Advanced Computational Fluid Dynamics ultra-detailed notes, zero-based leap improved, high-definition version of the text, you know ~ ~ ~
Platform: | Size: 1446912 | Author: fracatal | Hits:

[OtherAdvanced-Fuel-Cell-Modeling

Description: 国外最新计算流体力学文献,热点研究领域,最新前沿技术。 流体工程软件源代码开发人员的必备资料。-new CFD book in English version. all are about the most advanced methods. they are very help for the CFD source code developers.
Platform: | Size: 6625280 | Author: Mingming | Hits:

[OtherTurbulent-Particle-Laden-Gas-Flows

Description: 国外最新计算流体力学文献,热点研究领域,最新前沿技术。 流体工程软件源代码开发人员的必备资料。- new CFD book in English version. all are about the most advanced methods. they are very help for the CFD source code developers.
Platform: | Size: 2800640 | Author: Mingming | Hits:

[OtherTurbulent-Impinging-Jets-into-Porous

Description: 国外最新计算流体力学文献,热点研究领域,最新前沿技术。 流体工程软件源代码开发人员的必备资料。- new CFD book in English version. all are about the most advanced methods. they are very help for the CFD source code developers.
Platform: | Size: 4417536 | Author: Mingming | Hits:

[OtherModeling-for-Complex-Fluids

Description: 国外最新计算流体力学文献,热点研究领域,最新前沿技术。 流体工程软件源代码开发人员的必备资料。-new CFD book in English version. all are about the most advanced methods. they are very help for the CFD source code developers.
Platform: | Size: 3256320 | Author: Mingming | Hits:

[OtherNewl-Methods-for-Fluid-Dynamics

Description: 国外最新计算流体力学文献,热点研究领域,最新前沿技术。 流体工程软件源代码开发人员的必备资料。-new CFD book in English version. all are about the most advanced methods. they are very help for the CFD source code developers.
Platform: | Size: 5835776 | Author: Mingming | Hits:

[Mathimatics-Numerical algorithmszhangdeliang

Description: 中科院张德良教授编写的计算流体力学书附录里的代码-codes in the appendix of a CFD book written by zhang
Platform: | Size: 1326080 | Author: 沈杰 | Hits:

[Bookscomputational-fluid-dynamics--cfd--analysis-of-na

Description: In this book , a low-speed airfoil over the NACA 0012 airfoil at 2° and 14° attack angles with the given inlet velocity of 0.25 m/s, was modeled and computational fluid dynamic (CFD) analysis were performed using FLUENT in ANSYS. The Reynolds number based on the chord is roughly 𝑅 𝑒 = 2.88 × 106. The flow was modeled as incompressible and inviscid. All setup and procedures were done by following the steps provided Cornel University website. Though, mesh independence was achieved for 2° attack angle, for 14° attack angle which is more than the stall angle, mesh independence was not achieved. Lift and drag coefficient increases as the number of mesh element or the attack angle increases.-In this book , a low-speed airfoil over the NACA 0012 airfoil at 2° and 14° attack angles with the given inlet velocity of 0.25 m/s, was modeled and computational fluid dynamic (CFD) analysis were performed using FLUENT in ANSYS. The Reynolds number based on the chord is roughly 𝑅 𝑒 = 2.88 × 106. The flow was modeled as incompressible and inviscid. All setup and procedures were done by following the steps provided Cornel University website. Though, mesh independence was achieved for 2° attack angle, for 14° attack angle which is more than the stall angle, mesh independence was not achieved. Lift and drag coefficient increases as the number of mesh element or the attack angle increases.
Platform: | Size: 3686400 | Author: ahmed | Hits:

[Othercfd-SOLUTION

Description: 本书详细介绍了CFD数学算法,对于编程者有很大意义-This book details the CFD mathematical algorithms for the programmer a lot of sense
Platform: | Size: 23249920 | Author: 张美华 | Hits:

[Bookscfd

Description: book on computational fluid
Platform: | Size: 1853440 | Author: chottu | Hits:

[Other燃烧过程数值模拟教程

Description: 用于燃烧过程数值模拟的参考文件,实际工程也能用(CFD simulation for fuel combustion with software)
Platform: | Size: 1645568 | Author: Lucas zhang | Hits:

[Mathimatics-Numerical algorithmsCFD code in Matlab for anderson

Description: Anderson CFD 计算流体力学书中的matlab代码。(Anderson CFD Matlab code in CFD book.)
Platform: | Size: 102400 | Author: wyb20100828 | Hits:
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