LI Y H, HUANG Y, WANG Y Q. Wing-body thickness effects on aerodynamic and vortex flow characteristics of common low-aspect-ratio flying-wing configuration at transonic flow[J]. Acta Aerodynamica Sinica, 2015, 33(3):302-306. (in Chinese)

SHEN L C, ZHU H Y, NIU Y F. A survey of unmanned combat aircraft system development from X-47B[J]. National Defense Science Technology, 2013, 34(5):28-36. (in Chinese)

HU T Y. Multidisciplinary design optimization for flying wing aircraft preliminary design[D]. Nanjing University of Aeronautics and Astronautics. (in Chinese)

Daniel Dougherty, Adam Vore, Hamid Hefazi. High lift flap system for a tailless transport aircraft[R]. AIAA 2013-0965.

WANG Y X, ZHU X P, ZHOU Z. A control method of flying wing UAV for penetration of microburst[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(5):1673-1683. (in Chinese)

SHAN J X, HUANG Y, SU J C. Effect of the novel embedded control surfaces on direction control characteristic of low-aspect-ratio flying-wing configuration[J]. Acta Aerodynamica Sinica, 2015, 33(3):296-301. (in Chinese)

WU J F, QIN Y M, HUANG Z. Low speed experiment on longitudinal and lateral aerodynamic characteristics of the low aspect ratio flying wing calibration model[J]. Acta Aerodynamica Sinica, 2016, 34(1):125-130. (in Chinese)

KONG Y N, HE K F, WANG L X. Simulation of flying wing aircraft maneuver with leading edge jet control[J]. Acta Aerodynamica Sinica, 2013, 31(3):186-191. (in Chinese)

LIU S M, SUN J, LIU Z J. Research on flight control technology of the high-aspect-ratio flying wing model aircraft[J]. Flight dynamics, 2013, 31(6):558-560. (in Chinese)

MA C, WANG L X. Take-off and landing features of flying-wing configuration fighter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(4):429-433. (in Chinese)

KANG H. Belly flap innovation for blended-wing body[J]. International Aviation, 2008, 2:47. (in Chinese)

JAMES CHUNG, ERIC HALLBERG. Landing pitch control analysis for a blended wing body UCAV[R]. AIAA 2010-1035.

YANN D STAELENS, RON F BLACKWELDER. Novel pitch control effectors for a blended wing body airplane in takeoff and landing configuration[R]. AIAA 2007-68.

DANIEL DOUGHERTY, ADAM VORE, HAMID HEFAZI. High lift flap system for a tailless transport aircraft[R]. AIAA 2013-0965.

LU Y, ZHANG S G, LI X Q. A hazard analysis-based approach to improve the landing safety of a BWB remotely piloted vehicle[J]. Chinese Journal of Aeronautics, 2012, 25:846-853.

SHEN D, ZHANG B Q. Computational investigation on belly-flap for aerofoil[J]. Mechanical Science and Technology for Aerospace Engineering, 2012, 31(2):224-228.(in Chinese)