大攻角飞行平衡的数值研究

2015 17th International Symposium on Symbolic and Numeric Algorithms for Scientific Computing (SYNASC) Pub Date : 2015-09-21 DOI:10.1109/SYNASC.2015.22

A. Fortis, S. Balint

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引用次数: 0

摘要

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

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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2015 17th International Symposium on Symbolic and Numeric Algorithms for Scientific Computing (SYNASC)

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