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| 前机身对飞机大迎角气动特性的影响 | |
| 引用本文： | 刘国库,孙颖,周继良.前机身对飞机大迎角气动特性的影响[J].飞机设计,2011,31(6):6-9,15. |
| 作者姓名： | 刘国库 孙颖 周继良 |
| 作者单位： | 1. 中国人民解放军海军驻沈阳地区航空军事代表室,辽宁沈阳,110034 2. 中国人民解放军驻沈阳飞机工业（集团）有限公司军事代表室,辽宁沈阳,110034 3. 沈阳飞机设计研究所,辽宁沈阳,110035 |
| 摘 要： | 通过对一些相关文献的分析，得出了前机身外形是要求具有过失速机动能力的飞机气动设计的关键这一结论，并建议在气动布局工作中加强对前机身特性研究。 |
| 关 键 词： | 前机身 大迎角 过失速 |
Influence of Forebody on Aerodynamic Characteristics of Aircraft High Angles of Attack |
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| LIU Guo-ku,SUN Ying,ZHOU Ji-liang.Influence of Forebody on Aerodynamic Characteristics of Aircraft High Angles of Attack[J].Aircraft Design,2011,31(6):6-9,15. | |
| Authors: | LIU Guo-ku SUN Ying ZHOU Ji-liang |
| Institution: | 1. PLA Aeronautical Military Commisssary Office of Navy in Shenyang Region, Shenyang 110034, China ) ( 2. PLA Military Represensative Office in Shenyang Aircraft Industries (group) Co. Ltd., Shenyang 110034, China ) ( 3. Shenyang Aircraft Design ＆ Research Institute, Shenyang 110035, China ) |
| Abstract: | By analyzing series of relative research of aircrafts with good high AOA characteristic, conclusion is made that the forebody design is the key factor of aircraft aerodynamic design that require post-stall maneuver. Recommendation is also made on the future research of forebody design on aircraft configuration research. |
| Keywords: | forebody high angles of attack poststall |
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