APA引文

Wan Razali, W. M. H. (2009). Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali.

Chicago Style (17th ed.) Citation

Wan Razali, Wan Mohd Hafizan. Experimental Aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with Elevator Deflection of +15° and -15° Using Wind Tunnel (Mach Number 0.1-0.15) / Wan Mohd Hafizan Wan Razali. 2009.

MLA引文

Wan Razali, Wan Mohd Hafizan. Experimental Aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with Elevator Deflection of +15° and -15° Using Wind Tunnel (Mach Number 0.1-0.15) / Wan Mohd Hafizan Wan Razali. 2009.