| 翼型在自适应壁风洞中试验时的侧壁边界层三元效应研究 |
| |
| 引用本文： | 贺家驹,左培初,A·海德格特,E·司丹纽斯基.翼型在自适应壁风洞中试验时的侧壁边界层三元效应研究[J].实验流体力学,2001,15(2):16-27. |
| |
| 作者姓名： | 贺家驹 左培初 A·海德格特 E·司丹纽斯基 |
| |
| 作者单位： | 1. 西北工业大学空气动力研究室,
2. 德国宇航院哥廷根流体力学研究所, |
| |
| 摘 要： | 二元翼型试验时模型安装于侧壁转盘上会引起侧壁边界层三元效应，中国航空研究院西北工业大学和德国宇航院哥廷根流体力学研究所合作用计算和试验方法进行了研究。作者介绍了1995～1998年的研究，包含研究目的，方案，计算方法，在德国路德维希管风洞中的验证试验，结果分析和初步结论。
|
| 关 键 词： | 自适应壁风洞 翼型试验 边界层效应 洞壁干扰 |
| 文章编号： | 1007-3124(2001)02-0016-12 |
| 修稿时间： | 2000年11月7日 |
Research on side-wall
boundary layer three dimensional effect in airfoil testing with adaptive wall wind tunnel |
| |
| HE Jia-ju,ZUO Pei-chu,A·海德格特,E·司丹纽斯基.Research on side-wall
boundary layer three dimensional effect in airfoil testing with adaptive wall wind tunnel[J].Experiments and Measur in Fluid Mechanics,2001,15(2):16-27. |
| |
| Authors: | HE Jia-ju ZUO Pei-chu A·海德格特 E·司丹纽斯基 |
| |
| Institution: | HE Jia ju 1,ZUO Pei chu 1,A.Heddergott 2,E.Stanewsky 2 |
| |
| Abstract: | In two dimensional airfoil tests for models mounted on the side wall turn table may introduce three dimensional side wall boundary layer effects.CAE and DLR had done a cooperative research on this topic by calculating and measuring method to research the condition of three dimensional boundary layer effects on side wall.This paper describes the work that had been carried out since 1995～1998,including the research object and strategy,calculating method,tests in KRG for verifying and the analysis of the results as well as the primary conclusion. |
| |
| Keywords: | adaptive wall wind tunnel airfoil tests boundary layer effects wall interference |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
