Applied Aerodynamics Drag Prediction Workshop - NASA
2001年6月10日 · The DLR-F4 test cases have been chosen that address a subsonic wing/body transport configuration flying at subsonic through transonic speeds. The prediction of drag …
DLR-F4 Wing Body Redeker, G., “DLR-F4 Wing-Body Configuration,” A Selection of Experimental Test Cases for the Validation of CFD codes, AGARD Report AR-303, Aug. 1994.
Notes on Preparation of Geometry - NASA
2002年11月6日 · IGES file: dlr-f4.iges, 586KB. NASA Official Responsible for Content Dr. Neal T. Frink. Last Updated November 6, 2002.
Winglet Geometry Impact on DLR-F4 Aerodynamics and an Analysis …
In this article, the growth of aerodynamic efficiency and the growth of the wing structural stress is studied for DLR-F4 typical transport aircraft wing-body, after installing classical Whitcomb …
DLR-F4翼身组合体流场数值模拟 - 道客巴巴
2015年8月7日 · 使用“ 超立方体” 概念构 建绕 DLR— F4 翼身组合体的高质量多块结构拼接网格 ， 通过网格细分来研究网格密度对计算结果的影响．. 结果表明： 湍 流模型和网格密度对升力影 …
DLR-F4翼身组合体的数值分析 - 道客巴巴
2016年1月4日 · DLR．F4翼身组合体的数值分析王运涛，王光学，洪俊武，陈作斌中国空气动力研究与发展中心，四川绵阳621000 [摘要] 本文数值模拟了AIAA阻力计算工作小组提供的DLR …
The subject of this study is the DLR-F4 wing/body transonic model. Specifically, the work conducted herein was in support of the Iot CFD Drag Prediction Workshop, which was held in …
DLR-F4 Wing-Body Configuration. - Semantic Scholar
In this article, the growth of aerodynamic efficiency and the growth of the wing structural stress is studied for DLR-F4 typical transport aircraft wing-body, after installing classical Whitcomb …
Drag Prediction for the DLR-F4 Wing/Body using OVERFLOW and …
2002年1月1日 · The subject of this study is the DLR-F4 wing/body transonic model. Specifically, the work conducted herein was in support of the 1st CFD Drag Prediction Workshop, which …
Results from the Fourth AIAA Drag Prediction Workshop (DPW-IV) are summarized. The workshop focused on the prediction of both absolute and differential drag levels for wing-body …
- 某些结果已被删除