DocumentCode :
176625
Title :
Research on effect airwake acts on glide performance of carrier-based aircraft
Author :
Yu Yongtao ; Zhang Zhi
Author_Institution :
Acad. of Autom., Shenyang Aerosp. Univ., Shenyang, China
fYear :
2014
fDate :
May 31 2014-June 2 2014
Firstpage :
3532
Lastpage :
3537
Abstract :
The kinematic model of carrier-based aircraft was established. The airwake model described in USA military standard was introduced and analyzed. A landing simulation system was build based on the kinematic model of aircraft and airwake model. Numerical simulation was carried out to research the effect that airwake acted on the flight performance of carrier-base aircraft. Simulation results show that the gliding track of aircraft affected by airwake is lower than reference gliding track, which reduces the landing safety. The random component and free-air turbulence component of airwake own the dominate part of effect, the steady component makes contribution too, the periodic component acts little effect on aircraft. Airwake affects flight performance of aircraft by putting effect on the aerodynamic force of aircraft but not aero dynamical moment.
Keywords :
aerodynamics; aerospace computing; aircraft landing guidance; computational fluid dynamics; kinematics; turbulence; USA military standard; aerodynamic force; airwake model; carrier-based aircraft; free-air turbulence component; glide performance; gliding track; kinematic model; landing simulation system; periodic component; random component; steady component; Aircraft; Aircraft manufacture; Atmospheric modeling; Equations; Indexes; Mathematical model; Safety; Airwake; Carrier-based aircraft; Landing safety; Landing simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (2014 CCDC), The 26th Chinese
Conference_Location :
Changsha
Print_ISBN :
978-1-4799-3707-3
Type :
conf
DOI :
10.1109/CCDC.2014.6852791
Filename :
6852791
Link To Document :
بازگشت