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《Aircraft Design》 2007-05
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Application of Flying Wing Configuration to UCAV for Reconnaissance

ZAN Guang,LIU Yan-hua(Shenyang Aircraft Design & Research Institute,Shenyang 110035,China)  
Advantages in application of flying wing configuration to UCAV for reconnaissance are analyzed.Some major technical issues resulting from the application of flying wing configuration are discussed.Finally,it is suggested that the flying wing configuration is an optimal selection of aerodynamic configuration design of an UCAV for reconnaissance.
【CateGory Index】: V224
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Chinese Journal Full-text Database 10 Hits
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6 ZHANG Jian,ZHOU Zhou(College of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China);Correlation Analysis Between Gross and Performance Parameters of a Tactical UAV[J];Flight Dynamics;2009-04
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China Proceedings of conference Full-text Database 2 Hits
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7 ZHAN Guang,SUN Ying(Shenyan Aircraft Design & Research Institute,Shenyang 110035,China);Investigation on the Maneuverability of Uninhabited Combat Air Vehicle[J];Aircraft Design;2008-01
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【Secondary References】
Chinese Journal Full-text Database 3 Hits
1 Bao Junbo Wang Ganglin Wu Zhe(School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China);Optimization and experimental verification for aerodynamic scheme of flying-wing[J];Journal of Beijing University of Aeronautics and Astronautics;2012-02
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3 WANG Lei,WANG Lixin*,JIA Zhongren School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China;Control Allocation Method for Combat Flying Wing with Multiple Control Surfaces[J];Acta Aeronautica et Astronautica Sinica;2011-04
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