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.
توثيق أسلوب شيكاغو (الطبعة السابعة عشر)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.
توثيق جمعية اللغة المعاصرة MLA (الطبعة الثامنة)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.
تحذير: قد لا تكون هذه الاستشهادات دائما دقيقة بنسبة 100%.