APA引文

Che Wan Idris, C. W. Z. (2009). Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris.

Chicago Style (17th ed.) Citation

Che Wan Idris, Che Wan Zaidie. Experimental Aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with Elevator Deflection of +5° and -5° Using Wind Tunnel (Mach Number 0.1-0.15) / Che Wan Zaidie Che Wan Idris. 2009.

MLA引文

Che Wan Idris, Che Wan Zaidie. Experimental Aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with Elevator Deflection of +5° and -5° Using Wind Tunnel (Mach Number 0.1-0.15) / Che Wan Zaidie Che Wan Idris. 2009.