Development Of Design Of Aerofoil Shaped Fuselage And CFD Investigation Of Its Aerodynamic Characteristics

This paper explains about the computational design procedure for designing of an Unmanned Air Vehicles (UAV) having “Aerofoil Shaped Fuselage”. It also explains and analyses of the aerodynamic characteristics of an “Aerofoil Shaped Fuselage”. This model could be used for designing of the future UAV...

पूर्ण विवरण

ग्रंथसूची विवरण

मुख्य लेखकों:	Jahangir Alam, Wing Commander G.M., Mamun, Dr. Md., Abu. Taher Ali, Dr. Md., Sadrul Islam, Dr. A. K. M.
स्वरूप:	लेख
भाषा:	अंग्रेज़ी
प्रकाशित:	R&D Wing, MIST 2015
विषय:	Unmanned Air Vehicles (UAV), Aerofoil Shaped Fuselage, Aerodynamic Characteristics, Lift Coefficient, Drag Coefficient
ऑनलाइन पहुंच:	http://hdl.handle.net/123456789/221
टैग:	टैग जोड़ें कोई टैग नहीं, इस रिकॉर्ड को टैग करने वाले पहले व्यक्ति बनें!