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连续式跨声速风洞大开角扩散段设计方法研究概述

李红喆 廖达雄 丛成华

实验流体力学2012,Vol.26Issue(6):59-65,7.
实验流体力学2012,Vol.26Issue(6):59-65,7.

连续式跨声速风洞大开角扩散段设计方法研究概述

A review of design methods of continuous transonic wind tunnel's wide-angle diffuser

李红喆 1廖达雄 1丛成华1

作者信息

  • 1. 中国空气动力研究与发展中心空气动力学国家重点实验室,四川绵阳621000
  • 折叠

摘要

Abstract

The startup of large airplane project is starving for fine capability of capital continuous transonic wind tunnel facility. Wide-angle diffuser reduces the scale of the wind tunnel, but results in flow separation. The disposal and design of this section are important. This paper expatiates the effect of wide-angle diffuser, and then introduces its application instances oversea and ordinary disposal position. Emphasis on the design methods of screens in wide-angle diffuser to summarize a most optimized design scheme. Finally, puts forward some advises for the design of wide-angle diffuser in national continuous transonic wind tunnel.

关键词

跨声速/连续式风洞/大开角扩散段/阻尼网/设计

Key words

transonic/continuous wind tunnel/wide-angle diffuser/screen/design

分类

航空航天

引用本文复制引用

李红喆,廖达雄,丛成华..连续式跨声速风洞大开角扩散段设计方法研究概述[J].实验流体力学,2012,26(6):59-65,7.

基金项目

空气动力学国家重点实验室基金(JBKY11040401) (JBKY11040401)

实验流体力学

OA北大核心CSCDCSTPCD

1672-9897

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