Computational investigation on aerodynamic and stability characteristics of a vertical take-off and landing micro air vehicle

This research focuses on the numerical investigation of the aerodynamic and stability characteristics of a Vertical Takeoff and Landing (VTOL) Micro Air Vehicle (MAV). The numerical investigation is divided into two parts: statics and dynamics. In the static analysis, the full configuration of the V...

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Bibliographic Details
Main Author: Tobing, Sheila
Other Authors: Go Tiauw Hiong, Yongki
Format: Theses and Dissertations
Language:English
Published: 2009
Subjects:
Online Access:https://hdl.handle.net/10356/19014
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Institution: Nanyang Technological University
Language: English