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C_(nβ.dyn)作为大迎角稳定性判据的分析
引用本文:何植岱. C_(nβ.dyn)作为大迎角稳定性判据的分析[J]. 航空学报, 1988, 10(10): 462-468
作者姓名:何植岱
作者单位:西北工业大学
摘    要:
 本文通过具体算便分析了C_(n β.d y x)迎角稳定性判据的可靠性,对使用这一判据可能造成失误的原因作了归纳,得出了一些便于使用这一判据的结论。

收稿时间:1987-05-21;

THE ROLE OF CnB.dyn IN THE AIRCRAFT STABILITY AT HIGH ANGLES OF ATTACK
Northwestern Polytechnical University He Zhidai. THE ROLE OF CnB.dyn IN THE AIRCRAFT STABILITY AT HIGH ANGLES OF ATTACK[J]. Acta Aeronautica et Astronautica Sinica, 1988, 10(10): 462-468
Authors:Northwestern Polytechnical University He Zhidai
Affiliation:Northwestern Polytechnical University He Zhidai
Abstract:
In order to predict the aircraft stability'at high-angles-of-attack,some criteria were suggested and cnB.dyn is one of the most important criteria. Some surveys.about correlations of CnB.dyn with flight tests and authors opinion, the divergence can be predicted in most cases when Ca.dyn is negative. An example is'given to explain the effects of some of the aerodynamic derivatives on the aircraft stability.These derivatives are connected with GnB,dyn. Time history studies are carried out in this paper by programming, on a digital computer, a set offequations of motion pertinent to a typical fighter,by varying some of the aerodynamic derivations in a prede-terminate manner, and by observing the responses of some of the variables of mot ion to derivatives applied to the set of equations. From the calculating results, we can see that the aircraft could be unstable at high-angles-of-attack even the criterion is still satisfied, In the last part of this paper, we try to give some reasons to explain why these exceptions do exist.
Keywords:Stability at high-angle-of-attack   aeronautics derivatives.
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