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运输类飞机巡航阻力CFD计算分析

李权 郭兆电 邓一菊 廖振荣

航空工程进展2011,Vol.2Issue(4):402-408,7.
航空工程进展2011,Vol.2Issue(4):402-408,7.

运输类飞机巡航阻力CFD计算分析

CFD Analysis for Transport's Cruise Drag Prediction

李权 1郭兆电 1邓一菊 1廖振荣1

作者信息

  • 1. 中国航空工业集团公司第一飞机设计研究院,西安710089
  • 折叠

摘要

Abstract

For the accurate prediction of cruise drag in transport designing, a CFD analysis for the typical transport aircraft DLR_F6 wing-body configuration which was supplied by AIAA drag prediction workshop is put in practice, with "CCFD-MB", a large parallelized Reynolds averaged Navier-Stokes solver for multi-block structured grid; the effects of different meshes and different turbulence models on calculation results are compared; then a correction on DLR_F6 wing-body cruise drag which is from wind tunnel test is performed through comprehensive analysis of DLR F4 wing-body and relevant literature's results. It shows that the CFD results of DLR_F6 wing-body are more reliable than test data; CCFD-MB is an accurate flow solver and CFD is very positive for verifying the tunnel experiment.

关键词

巡航阻力预测/运输类飞机/CFD/DLR_F6翼身构型

Key words

cruise drag prediction/tansport aircraft/CFD/DLR_F6 wing body configuration

分类

航空航天

引用本文复制引用

李权,郭兆电,邓一菊,廖振荣..运输类飞机巡航阻力CFD计算分析[J].航空工程进展,2011,2(4):402-408,7.

基金项目

国家高技术研究发展计划资助 ()

航空工程进展

1674-8190

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