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...
Main Authors: | Mehmet Altun, İbrahim İyigün |
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Format: | Article |
Language: | English |
Published: |
Hezarfen Aeronautics and Space Technologies Institue
2004-01-01
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Series: | Havacılık ve Uzay Teknolojileri Dergisi |
Subjects: | |
Online Access: | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/93/85 |
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