SAE J 2966-2013
使用计算流体动力学中型和重型商用地面车辆空气动力学评估指南

Guidelines for Aerodynamic Assessment of Medium and Heavy Commercial Ground Vehicles Using Computational Fluid Dynamics

SAE J 2966-2013 发布历史

This document outlines general requirements for the use of CFD methods for aerodynamic simulation of medium and heavy commercial ground vehicles weighing more than 10 000lbs. The document provides guidance for aerodynamic simulation with CFD methods to support current vehicle characterization, vehicle development, vehicle concept development and vehicle component development. The guidelines presented in the document are related to Navier-Stokes and Lattice-Boltzmann based solvers. This document is only valid for the classes of CFD methods and applications mentioned. Other classes of methods and applications may or may not be appropriate to simulate the aero

SAE J 2966-2013由美国机动车工程师协会 US-SAE 发布于 2013-09-17。

SAE J 2966-2013在国际标准分类中归属于: 43.080.01 商用车辆综合,49.100 地面服务和维修设备。

SAE J 2966-2013 发布之时，引用了标准

• SAE J 1252-2012 卡车和客车的SAE风洞试验规程

SAE J 2966-2013的历代版本如下：

• 2013年09月17日 SAE J 2966-2013 使用计算流体动力学中型和重型商用地面车辆空气动力学评估指南
• 2021年06月01日 SAE J 2966-2021

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标准号

SAE J 2966-2013

发布日期

2013年09月17日

实施日期

废止日期

无

国际标准分类号

43.080.01;49.100

发布单位

US-SAE

引用标准

ASME AMR V.62.4 ASME JFE V. 130 ASME V&V20 SAE J 1252-2012 2006-01-3544 2007-01-4295 2009-01-1167 2010-01-0756 2012-01-0106 2012-01-0107 AIAA-G-077 AIAA 93-2906 AIAA 98-3007 AIAA 2000-2306 R-177

适用范围

This document outlines general requirements for the use of CFD methods for aerodynamic simulation of medium and heavy commercial ground vehicles weighing more than 10 000lbs. The document provides guidance for aerodynamic simulation with CFD methods to support current vehicle characterization, vehicle development, vehicle concept development and vehicle component development. The guidelines presented in the document are related to Navier-Stokes and Lattice-Boltzmann based solvers. This document is only valid for the classes of CFD methods and applications mentioned. Other classes of methods and applications may or may not be appropriate to simulate the aero