CANARD

作品数：35被引量：54H指数：4
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Effect of longitudinal lift distribution on sonic boom of a canard-wing-stabilator-body configuration被引量：1
《Chinese Journal of Aeronautics》2023年第6期92-108,共17页Liwen ZHANG Zhonghua HAN Jianling QIAO Wenping SONG Yulin DING Xuehe WANG 
sponsored by the National Natural Science Foundation of China(Nos.12072285,U20B2007);the Shaanxi Science Fund for Distinguished Young Scholars,China(No.2020JC-13);the Natural Science Funding of Shaanxi Province,China(No.2020JM-127).
After the last flight of the Concorde in 2003,sonic boom has been one of the obstacles to the return of a supersonic transport aircraft to service.To reduce the sonic boom intensity to an acceptable level,it is of gre...
关键词：Computational fluid dynamics Longitudinal lift distribution Sonic boom Sonic boom reduction Supersonic transport 
Flight dynamics characteristics of canard rotor/wing aircraft in helicopter flight mode被引量：4
《Chinese Journal of Aeronautics》2019年第7期1577-1587,共11页Honggang GAO Ao HE Zhenghong GAO Yang NA Yangping DENG 
The aerodynamic layout of the Canard Rotor/Wing(CRW) aircraft in helicopter flight mode differs significantly from that of conventional helicopters. In order to study the flight dynamics characteristics of CRW aircraf...
关键词：CANARD rotor/wing AIRCRAFT DYNAMICS analysis FLIGHT DYNAMICS HELICOPTER LINEARIZATION Model building 
Observer-based adaptive sliding mode backstepping output-feedback DSC for spin-stabilized canard-controlled projectiles被引量：5
《Chinese Journal of Aeronautics》2017年第3期1115-1126,共12页Yuanchuan SHEN Jianqiao YU Guanchen LUO Xiaolin AI Zhenyue JIA Fangzheng CHEN 
supported by the National Natural Science Foundation of China(No.11532002)
This article presents a complete nonlinear controller design for a class of spin-stabilized canard-controlled projectiles.Uniformly ultimate boundedness and tracking are achieved,exploiting a heavily coupled,bounded u...
关键词：Backstepping Dynamic surface control technique Nonlinear systems Observers Sliding mode control Spin-stabilized canard controlled projectiles 
Aeroservoelastic modeling and analysis of a canard-configured air-breathing hypersonic vehicles被引量：8
《Chinese Journal of Aeronautics》2013年第4期831-840,共10页Zeng Kaichun Xiang Jinwu Li Daochun 
co-supported by the National Natural Science Foundation of China(Nos.90916006,91116019 and 91216102)
Air-breathing hypersonic vehicles （HSVs） are typically characterized by interactions of elasticity, propulsion and rigid-body flight dynamics, which may result in intractable aeroservoelastic problem. When canard is...
关键词：Aeroservoelasticity Canard Flight dynamics Hypersonic vehicles Pivot Stability 
Closed-loop dynamic control allocation for aircraft with multiple actuators被引量：5
《Chinese Journal of Aeronautics》2013年第3期676-686,共11页Gai Wendong Wang Honglun 
Program for New Century Excellent Talents in University (NCET-10-0032)
A closed-loop control allocation method is proposed for a class of aircraft with multiple actuators. Nonlinear dynamic inversion is used to design the baseline attitude controller and derive the desired moment increme...
关键词：Canard rotor/wing aircraft Closed-loop control allocation Dynamic inversion Flight control systems Redundant actuators 
Numerical Simulation of Rotor-aerodynamic Surface Interaction in Hover Using Moving Chimera Grid被引量：3
《Chinese Journal of Aeronautics》2012年第3期342-348,共7页LI Yibo MA Dongli 
Three-dimensional unsteady Navier-Stokes equations are numerically solved to simulate the aerodynamic interaction of rotor, canard and horizontal tail in hover based on moving chimera grid. The variations of unsteady ...
关键词：unsteady flow chimera grid canard rotor/wing aerodynamic interaction numerical simulation 
Investigation of Vortex Interaction in Canard-FSW Configurations Based on the Numerical Wind Tunnel Method被引量：1
《Chinese Journal of Aeronautics》2010年第3期312-319,共8页张国庆 杨树兴 徐勇 
National Defense Basic Research Program (B222006060)
The vortex interference mechanism on low Reynolds number between the canard and main wing of the canard-forward sweep wing （Canard-FSW） configurations is simulated numerically by employing the numerical wind tunnel ...
关键词：cluster system Canard-FSW backward sweep canard forward sweep canard VORTEX interaction mesh 
Aerodynamic Design for Three-Dimensional Multi-lifting Surfaces at Transonic Flow被引量：2
《Chinese Journal of Aeronautics》2006年第1期24-30,共7页杨青真 张仲寅 Thomas Streit Georg Wichmann 郑勇 
ChinaGermanyAeronauticTechnologyCooperationProject(CAEDLRCooperationTopic200303).
An aerodynamic design method and corresponding codes are developed for three-dimensional multi lifting surfaces at transonic flow. It is based on the ＂iterative residual correction＂ concept that is successfully used...
关键词：aerodynamic design transonic flow iterative residual correction multi-liftlng surfaces CANARD WING 
THE CANARD-WING INTERFERENCE AND STALL SAFETY OF LIGHT CANARD AIRCRAFT
《Chinese Journal of Aeronautics》1991年第2期226-234,共9页Bai Zhenzhu Xie Xiaobin Nanjing Aeronautical Institute Nanjing 210016, P.R.C 
In this article, the interference between canard and wing is discussed on the basis of wind-tunnel test, with a brief review of the development of aerodynamic configurations of AD-100 / 200 (two light canard aircraft ...
关键词：In than THE CANARD-WING INTERFERENCE AND STALL SAFETY OF LIGHT CANARD AIRCRAFT down AOA 
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