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.
Chicago Style (17th ed.) CitationJundam, 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.
MLA引文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.
警告：这些引文格式不一定是100％准确.