Estimation of Stability Parameters for Wide Body Aircraft Using Computational Techniques

Estimation of Stability Parameters for Wide Body Aircraft Using Computational Techniques

In this paper, we present the procedure of estimating the aerodynamic coefficients for a commercial aviation aircraft from geometric parameters at low-cruise-flight conditions using US DATCOM (United States Data Compendium) and XFLR software. The purpose of this research was to compare the stability...

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Bibliographic Details
Main Authors: Muhammad Ahmad, Zukhruf Liaqat Hussain, Syed Irtiza Ali Shah, Taimur Ali Shams
Format: Article
Language:English
Published: MDPI AG 2021-02-01
Series:Applied Sciences
Subjects:
aerodynamic coefficients
Boeing
DATCOM
stability and control
XFLR
Online Access:https://www.mdpi.com/2076-3417/11/5/2087

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