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�������պ����ѧѧ�� 2009, Vol. 35 Issue (4) :429-433    DOI:
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Take-off and landing features of flying-wing configuration fighter
Ma Chao, Wang Lixin*
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

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Abstract�� Innovative control surfaces are implemented on the flying-wing configuration combat aircraft, and the flaps of traditional aircraft which are used for lift increasing during take-off and landing are canceled. The control principles during take-off and landing were summarized. A flying-wing configuration aircraft was chosen for instant, so the low-speed aerodynamic characteristics of the typical flying-wing configuration aircraft were compared with conventional aircraft based on results of tunnel tests. Then the performances of take-off and landing were calculated and compared with typical traditional fighter F-16. The results prove that, the inherent feature of all-wing design brings low wing-load, which makes take-off and landing performances of flying-wing configuration fighter easy to satisfy. The valuable references were provided for estimating the battle effectiveness and designing of flying-wing configuration fighter.
Keywords�� flying-wing configuration   control characteristic   flight performance   take-off and landing     
Received 2008-04-08;
Fund:

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About author: �� ��(1983-),��,�����ϲ���,��ʿ��,machao@ase.buaa.edu.cn.
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Ma Chao, Wang Lixin.Take-off and landing features of flying-wing configuration fighter[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2009,V35(4): 429-433
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