A study on the circular planform unmanned aerial vehicle /
In this work, aerodynamics investigation of the flow around the circular planform unmanned aerial vehicle (CP-UAV) was carried out numerically and validated with existencing published experimental data. The aircraft uses NACA 4412 airfoil. CD-Adapco STARCCM+ CFD software was used to simulate the flo...
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主要作者: | Mohamed Ali Suliman, Suliman Mohamed |
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格式: | Thesis |
语言: | English |
出版: |
Kuala Lumpur :
Kulliyyah of Engineering, International Islamic University Malaysia,
2014
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在线阅读: | http://studentrepo.iium.edu.my/handle/123456789/4893 |
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