Numerical Investigations of Equilibriums in a Flight with High Angle of Attack

A. Fortis, S. Balint
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Abstract

This paper is a case study which presents numericalinvestigations based on the theoretical background developed in [1]. The purpose is to numerically investigate the existence and the stability of equilibriums, as well as the existence of possible bifurcation at an equilibrium point for a set of given aero-dynamic data. The computations are performed in the framework of the non-simplified Aero-Data Model in a Research Environment, when the angle of attack is high.
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大攻角飞行平衡的数值研究
本文是一个案例研究,在[1]中发展的理论背景的基础上进行数值调查。目的是数值研究一组给定气动数据平衡点的存在性和稳定性,以及平衡点上可能的分支的存在性。在某研究环境下,当迎角较大时,在非简化航空数据模型框架下进行计算。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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