Investigation of the Aerodynamic Characteristics of an Aerofoil Shaped Fuselage UAV Model-Reference-Cited by-同舟云学术

Investigation of the Aerodynamic Characteristics of an Aerofoil Shaped Fuselage UAV Model

Published:2014 Issue: Volume:90 Page:225-231
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Alam G.M. Jahangir,Mamun Md.,Ali Md. Abu. Taher,Islam Md. Quamrul,Islam A.K.M. Sadrul

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference4 articles.

1. Development of Design of Aerofoil Shaped Fuselage and CFD Investigation of its Aerodynamic Characteristics”;Jahangir Alam;MIST Journal of Science and Technology,2013

2. Autonomous Vehicle Technologies for Small Fixed-Wing UAVs;Randal;Journal of Aerospace Computing, Information and Communication,2005

3. Design of a Morphing Airfoil for a Light Unmanned Aerial Vehicle using High-Fidelity Aerodynamic Shape Optimization;Secanell;Journal of American Institute of Aeronautics and Astronautics (AIAA 2005-1891),2005

4. Improved Aerodynamic Characteristics of Aerofoil Shaped Fuselage than that of the Conventional Cylindrical Shaped Fuselage”;Jahangir Alam;International Journal of Scientific & Engineering Research,2013

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