Jundam, M. F. (2009). Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam.
توثيق أسلوب شيكاغو (الطبعة السابعة عشر)Jundam, Mohd. Fazil. Computational Fluid Dynamics (CFD) Analysis of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with Elevator Deflection of - 15° (upward) at 0.1 and 0.3 Mach Number / Mohd. Fazil Jundam. 2009.
توثيق جمعية اللغة المعاصرة MLA (الطبعة الثامنة)Jundam, Mohd. Fazil. Computational Fluid Dynamics (CFD) Analysis of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with Elevator Deflection of - 15° (upward) at 0.1 and 0.3 Mach Number / Mohd. Fazil Jundam. 2009.
تحذير: قد لا تكون هذه الاستشهادات دائما دقيقة بنسبة 100%.