TAIL

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  • 期刊=Transactions of Nanjing University of Aeronautics and Astronauticsx
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Transition Stage Control of Tail Sitter Aircraft Based on Guardian Maps
《Transactions of Nanjing University of Aeronautics and Astronautics》2020年第2期322-331,共10页ZHANG Yong CHEN Xinyi 
This work was supported by the Fundamental Research Funds for the Central Universities(No.NJ2018015)。
To deal with the high nonlinearities and strong couplings in the transition stage of tailsitter aircraft,an adaptive gainscheduling controller is proposed by combining the guardian maps theory and H∞control theory.Th...
关键词：tailsitter aircraft transition stage guardian maps adaptive gainscheduling controller 
Simulation on Helicopter Scissors Tail-Rotor Noise Based on N-S Equations and F1A Formulas
《Transactions of Nanjing University of Aeronautics and Astronautics》2017年第6期710-719,共10页Meng Xiaowei Xu Guohua Shi Yongjie Wang Liangquan 
Aiming at the noise of helicopter scissors tail-rotor,an advanced numerical method is established by combining computational fluid dynamics(CFD)model with Farassat 1 A(F1 A)formula.In this method,Navier-tokes(N-S)equa...
关键词：FW-H equation scissors tail rotor thickness noise loading noise HELICOPTER computational fluid dynamics(CFD) 
Numerical Calculations of Aerodynamic and Acoustic Characteristics for Scissor Tail-Rotor in Forward Flight被引量：4
《Transactions of Nanjing University of Aeronautics and Astronautics》2016年第3期285-293,共9页Fan Feng Huang Shuilin Lin Yongfeng 
The aerodynamic and aeroacoustic characteristics of a scissor tail-rotor in a forward flight are numerically calculated.A novel computational fluid dynamics(CFD)model based on Navier-Stokes(N-S)equations is presented ...
关键词：computational fluid dynamics(CFD) scissor tail-rotors aerodynamic characteristics aeroacoustic characteristics Navier-Stokes(N-S)equations 
PARAMETER ANALYSIS ON CIRCULATION CONTROLLED CIRCULAR CYLINDER FOR NOTAR^TM TAIL BOOM被引量：1
《Transactions of Nanjing University of Aeronautics and Astronautics》2013年第3期282-291,共10页李家春 杨卫东 高宁 
Lift on circulation control(CC)circular cylinder is calculated via numerical simulations based on 2Drealizable k-εepsilon viscous model and compared with experimental data.The simulation result shows an acceptable ag...
关键词：HELICOPTER AERODYNAMICS NOTARTM circulation control 
ANALYSIS OF WORKING MODES OF HYBRID EXCITATION DOUBLY SALIENT MOTOR被引量：3
《Transactions of Nanjing University of Aeronautics and Astronautics》2006年第4期264-271,共8页秦海鸿 赵志英 龚春英 严仰光 
国家自然科学基金(50337030)资助项目。~~
A more accurate analysis method on working modes is proposed by considering the winding terminal voltage and the eondueting power device as state parameters. For the three-phase hybrid excitation doubly salient machi...
关键词：hybrid excitation doubly salient motor working mode COMMUTATION current tail 
AERODYNAMIC ANALYSIS OF HELICOPTER SHROUDED TAIL ROTOR BY MOMENTUM THEORY
《Transactions of Nanjing University of Aeronautics and Astronautics》1998年第2期50-54,共5页徐国华 王适存 
In this paper, in order to clarify the gains of the shroud in the shrouded tail rotor system, a thrust division factor q , which represents the ratio of the shroud thrust to the total thrust of the shrouded tail ro...
关键词：helicopters tail rotors SHROUD aerodynamic analysis 
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