DocumentCode :
2741988
Title :
A New Method of Acquiring Compound Aerodynamic Data of a Kind of Flying Saucer
Author :
Gu, Wenjin ; Feng, Guohu ; Zhao, Hongchao
Author_Institution :
Res. Inst. of Vehicle´´s Control Syst., Naval Aeronaut. Eng. Inst., Yantai
Volume :
2
fYear :
0
fDate :
0-0 0
Firstpage :
8141
Lastpage :
8144
Abstract :
A kind of flying saucer can equivalently fly without the consideration of the effect of sideslip, because it has unique geometry shape. According to this character, its aerodynamic data of sideslip can be converted by aerodynamic data without sideslip. So it can largely reduce the number of wind tunnel test, and save the cost of test. This paper deducted the converting formula that gets aerodynamic data of sideslip from aerodynamic data without sideslip, and validated converting formula by numerical simulation, because the data calculated by the formula were consistent with the data got by numerical simulation. The form of converting formula is simple, and easily understood. It can be used for reference to the development of flying saucer
Keywords :
aerodynamics; aerospace simulation; data acquisition; numerical analysis; space vehicles; compound aerodynamic data acquisition; flying saucer; numerical simulation; sideslip; wind tunnel test; Aerodynamics; Aerospace engineering; Automation; Control systems; Costs; Geometry; Intelligent control; Numerical simulation; Shape control; Testing; effective angles of attack; equivalent flying; flying saucer; numerical simulation; sideslip;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on
Conference_Location :
Dalian
Print_ISBN :
1-4244-0332-4
Type :
conf
DOI :
10.1109/WCICA.2006.1713560
Filename :
1713560
Link To Document :
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