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.
توثيق أسلوب شيكاغو (الطبعة السابعة عشر)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.
توثيق جمعية اللغة المعاصرة MLA (الطبعة الثامنة)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.
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