Author: Qunzhen Wang
Publisher:
ISBN:
Category : Fluid dynamic measurements
Languages : en
Pages : 38
Book Description
USM3D is a widely-used unstructured flow solver for simulating inviscid and viscous flows over complex geometries. The current version (version 5.0) of USM3D, however, does not have advanced turbulence models to accurately simulate complicated flow. We have implemented two modified versions of the original Jones and Launder k-epsilon "two-equation" turbulence model and the Girimaji algebraic Reynold stress model in USM3D. Tests have been conducted for three flat plate boundary layer cases, a RAE2822 airfoil and an ONERA M6 wing. The results are compared with those from direct numerical simulation, empirical formulae, theoretical results, and the existing Spalart-Allmaras one-equation model
Implementation of Advanced Two Equation Turbulence Models in the USM3D Unstructured Flow Solver
Author: Qunzhen Wang
Publisher:
ISBN:
Category : Fluid dynamic measurements
Languages : en
Pages : 38
Book Description
USM3D is a widely-used unstructured flow solver for simulating inviscid and viscous flows over complex geometries. The current version (version 5.0) of USM3D, however, does not have advanced turbulence models to accurately simulate complicated flow. We have implemented two modified versions of the original Jones and Launder k-epsilon "two-equation" turbulence model and the Girimaji algebraic Reynold stress model in USM3D. Tests have been conducted for three flat plate boundary layer cases, a RAE2822 airfoil and an ONERA M6 wing. The results are compared with those from direct numerical simulation, empirical formulae, theoretical results, and the existing Spalart-Allmaras one-equation model
Publisher:
ISBN:
Category : Fluid dynamic measurements
Languages : en
Pages : 38
Book Description
USM3D is a widely-used unstructured flow solver for simulating inviscid and viscous flows over complex geometries. The current version (version 5.0) of USM3D, however, does not have advanced turbulence models to accurately simulate complicated flow. We have implemented two modified versions of the original Jones and Launder k-epsilon "two-equation" turbulence model and the Girimaji algebraic Reynold stress model in USM3D. Tests have been conducted for three flat plate boundary layer cases, a RAE2822 airfoil and an ONERA M6 wing. The results are compared with those from direct numerical simulation, empirical formulae, theoretical results, and the existing Spalart-Allmaras one-equation model
Implementation of Advanced Two Equation Turbulence Models in the Usm3d Unstructured Flow Solver
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781723730856
Category : Science
Languages : en
Pages : 38
Book Description
USM3D is a widely-used unstructured flow solver for simulating inviscid and viscous flows over complex geometries. The current version (version 5.0) of USM3D, however, does not have advanced turbulence models to accurately simulate complicated flow. We have implemented two modified versions of the original Jones and Launder k-epsilon "two-equation" turbulence model and the Girimaji algebraic Reynolds stress model in USM3D. Tests have been conducted for three flat plate boundary layer cases, a RAE2822 airfoil and an ONERA M6 wing. The results are compared with those from direct numerical simulation, empirical formulae, theoretical results, and the existing Spalart-Allmaras one-equation model.Wang, Qun-Zhen and Massey, Steven J. and Abdol-Hamid, Khaled S.Langley Research CenterAPPLICATIONS PROGRAMS (COMPUTERS); NAVIER-STOKES EQUATION; UNSTRUCTURED GRIDS (MATHEMATICS); TURBULENCE MODELS; AIRFOILS; WINGS; VISCOUS FLOW; FLAT PLATES; INVISCID FLOW; COMPUTERIZED SIMULATION; COMPUTATIONAL FLUID DYNAMICS; K-EPSILON TURBULENCE MODEL; REYNOLDS STRESS; STRESS ANALYSIS; FLOW DISTRIBUTION; FINITE VOLUME METHOD; VORTICES; EDDY VISCOSITY
Publisher: Independently Published
ISBN: 9781723730856
Category : Science
Languages : en
Pages : 38
Book Description
USM3D is a widely-used unstructured flow solver for simulating inviscid and viscous flows over complex geometries. The current version (version 5.0) of USM3D, however, does not have advanced turbulence models to accurately simulate complicated flow. We have implemented two modified versions of the original Jones and Launder k-epsilon "two-equation" turbulence model and the Girimaji algebraic Reynolds stress model in USM3D. Tests have been conducted for three flat plate boundary layer cases, a RAE2822 airfoil and an ONERA M6 wing. The results are compared with those from direct numerical simulation, empirical formulae, theoretical results, and the existing Spalart-Allmaras one-equation model.Wang, Qun-Zhen and Massey, Steven J. and Abdol-Hamid, Khaled S.Langley Research CenterAPPLICATIONS PROGRAMS (COMPUTERS); NAVIER-STOKES EQUATION; UNSTRUCTURED GRIDS (MATHEMATICS); TURBULENCE MODELS; AIRFOILS; WINGS; VISCOUS FLOW; FLAT PLATES; INVISCID FLOW; COMPUTERIZED SIMULATION; COMPUTATIONAL FLUID DYNAMICS; K-EPSILON TURBULENCE MODEL; REYNOLDS STRESS; STRESS ANALYSIS; FLOW DISTRIBUTION; FINITE VOLUME METHOD; VORTICES; EDDY VISCOSITY
AIAA Aerospace Sciences Meeting and Exhibit, 42nd
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 838
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 838
Book Description
NASA Langley Scientific and Technical Information Output 2000
37th AIAA Aerospace Sciences Meeting and Exhibit
International Aerospace Abstracts
Scientific and Technical Aerospace Reports
AIAA Guide for the Verification and Validation of Computational Fluid Dynamics Simulations
Author: American Institute of Aeronautics and Astronautics
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781563472855
Category : Computational fluid dynamics
Languages : en
Pages : 0
Book Description
This document defines a number of key terms, discusses fundamental concepts, and specifies general procedures for conducting verification and validation of computational fluid dynamics simulations. It's goal is to provide a foundation for the major issues and concepts in verification and validation. However, it does not recommend standards in these areas because a number of important issues are not yet resolved.
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781563472855
Category : Computational fluid dynamics
Languages : en
Pages : 0
Book Description
This document defines a number of key terms, discusses fundamental concepts, and specifies general procedures for conducting verification and validation of computational fluid dynamics simulations. It's goal is to provide a foundation for the major issues and concepts in verification and validation. However, it does not recommend standards in these areas because a number of important issues are not yet resolved.
Project Constellation
Author: Tim McElyea
Publisher: Apogee Books
ISBN: 9781894959490
Category : Manned space flight
Languages : en
Pages : 0
Book Description
Project Constellation is NASA's initiative to develop a replacement for the aging Space Shuttle. It's main goal is to provide spacecraft for returning to the Moon by the year 2020. This Pocket Space Guide, #9 in the series, gives the background information on how the program was formed and what it is destined to accomplish. Details are given for all of the elements of the Project Constellation, from the Lunar Precursor Robotic Program to the Orion spacecraft, Ares launch vehicles, and the Lunar Surface Access Module. Project Constellation is realizing President Bush's "Vision" for space and this book chronicles the progress and outlines the plans for tomorrow.
Publisher: Apogee Books
ISBN: 9781894959490
Category : Manned space flight
Languages : en
Pages : 0
Book Description
Project Constellation is NASA's initiative to develop a replacement for the aging Space Shuttle. It's main goal is to provide spacecraft for returning to the Moon by the year 2020. This Pocket Space Guide, #9 in the series, gives the background information on how the program was formed and what it is destined to accomplish. Details are given for all of the elements of the Project Constellation, from the Lunar Precursor Robotic Program to the Orion spacecraft, Ares launch vehicles, and the Lunar Surface Access Module. Project Constellation is realizing President Bush's "Vision" for space and this book chronicles the progress and outlines the plans for tomorrow.