Parametric geometry modeling of flying wing UAV configuration integrated with intake and exhaust
Flying wing is a preferred configuration for unmanned combat air vehicle（UCAV），in which its airframe is highly integrated with intake and exhaust of propulsion system. To implement rapid geometric model of flying wing UCAV concept，a parametric geometry modeling method for flying wing UCAV configurat...
| Main Authors: | , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2024-02-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://qktg.shnu.edu.cn/zrb/shsfqkszrb/ch/reader/view_abstract.aspx?file_no=2024-1-30.htm |