Unsteady aerodynamic investigation of the propeller-wing interaction for a rocket launched unmanned air vehicle

The aerodynamic characteristics of propeller-wing interaction for the rocket launched UAV have been investigated numerically by means of sliding mesh technology. The corresponding forces and moments have been collected for axial wing placements ranging from 0.056 to 0.5D and varied rotating speeds....

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Main Authors: Zhang, G. Q., Yu, S. C. M., Chien, A., Xu, Y.
其他作者: School of Mechanical and Aerospace Engineering
格式: Article
語言:English
出版: 2013
主題:
在線閱讀:https://hdl.handle.net/10356/105873
http://hdl.handle.net/10220/17941
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機構: Nanyang Technological University
語言: English