DYNAMIC STABILITY DERIVATIVES OF A MANUEVERING COMBAT AIRCRAFT MODEL

The purpose of this experimental study presented in this paper is to measure the dynamic stability derivatives of a generic combat aircraft model in the Ankara Wind Tunnel by using the direct forced oscillation technique. The model, which is used for the oscillatory tests is known as the AGARD, Stan...

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Bibliographic Details
Main Authors: Mehmet Altun, İbrahim İyigün
Format: Article
Language:English
Published: Turkish Air Force Academy 2004-01-01
Series:Havacılık ve Uzay Teknolojileri Dergisi
Subjects:
Online Access:http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/93/85