Design of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) engine nacelle / Asrul Azuwar Hashim
An engine nacelle is used to enclose the engine in a streamlined housing to improve the aerodynamics of the aircraft, to support and protect the engine and its component. For the preliminary of design the engine nacelle, an attempt to install the engine nacelle on the upper surface of the aircraft h...
محفوظ في:
المؤلف الرئيسي: | Hashim, Asrul Azuwar |
---|---|
التنسيق: | أطروحة |
اللغة: | English |
منشور في: |
2006
|
الموضوعات: | |
الوصول للمادة أونلاين: | https://ir.uitm.edu.my/id/eprint/37212/1/37212.pdf |
الوسوم: |
إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
مواد مشابهة
-
Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi
بواسطة: Abdulawi, Mohd Yusof Safaruddin
منشور في: (2006) -
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
بواسطة: Che Wan Idris, Che Wan Zaidie
منشور في: (2009) -
Estimation And Analysis Of Performance, Stability And Control For Unmanned Aerial Vehicle (Uav) Tamingsari Using Semiempirical Method
بواسطة: Arshad, Aizam Shahroni Mohd
منشور في: (2010) -
Numerical analysis of tubercles leading edge for unmanned aerial vehicle composite wing
بواسطة: Basri, Ernnie Illyani
منشور في: (2020) -
Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
بواسطة: Mohd Ali, Zurriati
منشور في: (2015)