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Trim Drag Prediction for Blended-Wing-Body UAV Configuration

Deng Haiqiang Yu Xiongqing Yin Hailian Deng Feng

南京航空航天大学学报（英文版）2015，Vol.32Issue(1)：133-136,4.

Trim Drag Prediction for Blended-Wing-Body UAV Configuration

Deng Haiqiang ¹Yu Xiongqing ²Yin Hailian ¹Deng Feng²

作者信息

1. UAV Research Institute, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China
2. Key Laboratory of Fundamental Science for National Defense Advanced Design Technology of Flight Vehicle,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China
折叠

摘要

关键词

aerodynamic configuration/blended-wing-body/trim drag/unmanned aerial vehicles (UAVs)

Key words

aerodynamic configuration/blended-wing-body/trim drag/unmanned aerial vehicles (UAVs)

分类

航空航天

引用本文复制引用

Deng Haiqiang,Yu Xiongqing,Yin Hailian,Deng Feng..Trim Drag Prediction for Blended-Wing-Body UAV Configuration[J].南京航空航天大学学报（英文版）,2015,32(1):133-136,4.

基金项目

This work was supported by the National Defense Basic Scientific Research Program of China (No.A2520110006)and the Fundamental Research Funds for the Central Universities (Nos.NJ20130001,NJ2012014). （No.A2520110006）

南京航空航天大学学报（英文版）

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ISSN：1005-1120

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