Development of a dynamic wind tunnel rig for aircraft pure pitching motion
This paper presents the design, fabrication and testing of a dynamic wind tunnel test rig that is used in conjunction with aircraft dynamics theory in estimating aerodynamics stability derivatives. The value of and can be obtained from free oscillation theory of pure pitching motion. The rig compris...
Saved in:
Main Authors: | Mansor, Shuhaimi, Ishak, Iskandar Shah, Ong, Meng Wei, Fahrurazi, Istas |
---|---|
格式: | Article |
语言: | English |
出版: |
Faculty of Mechanical Engineering
2000
|
主题: | |
在线阅读: | http://eprints.utm.my/id/eprint/8314/1/ShuhaimiMansor2000_DevelopmentofaDynamicWind.pdf http://eprints.utm.my/id/eprint/8314/ http://portal.psz.utm.my/psz/index.php?option=com_content&task=view&id=128&Itemid=305&PHPSESSID=81b664e998055f65b4ccff8f61bf7cb2 |
标签: |
添加标签
没有标签, 成为第一个标记此记录!
|
相似书籍
-
Subsonic wind tunnels in Malaysia: a review
由: Wiriadidjaja, Surjatin, et al.
出版: (2012) -
Wind tunnel testing of composite wing flutter speed due to control surface excitation
由: Iyas, M. M., et al.
出版: (2013) -
Aircraft rigid-body equation of motions: a non linear model
由: Legowo, Ari
出版: (2011) -
Wind Tunnel Experiment Of Aeroelastic Flutter
由: Mah, Chuen Tak
出版: (2018) -
Design, construction, and testing of an open-loop low-speed wind tunnel
由: Muhammad Adnin, Mat Bahari
出版: (2012)