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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Bibliographic Details
Main Authors: Zhang, G. Q., Yu, S. C. M., Chien, A., Xu, Y.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2013
Subjects:
Online Access:https://hdl.handle.net/10356/105873
http://hdl.handle.net/10220/17941
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Institution: Nanyang Technological University
Language: English

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