Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
The Blended Wing-Body (BWB) aircraft is an unconventional aircraft that offers the aerodynamics performance advantages compared to the conventional aircraft. This type of aircraft has a unique design where the main body is blended together with the wing that gives the additional lift of the aircraft...
محفوظ في:
المؤلف الرئيسي: | Mohd Ali, Zurriati |
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التنسيق: | أطروحة |
اللغة: | English |
منشور في: |
2015
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الموضوعات: | |
الوصول للمادة أونلاين: | https://ir.uitm.edu.my/id/eprint/15663/2/15663.pdf |
الوسوم: |
إضافة وسم
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مواد مشابهة
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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) -
Aerodynamic study on go-kart using computer aided tools / Mohd Yusri Abu Bakar
بواسطة: Abu Bakar, Mohd Yusri
منشور في: (2005) -
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) -
Aerodynamic characteristics of compound wing configuration of wing-in-ground effect vehicle
بواسطة: Jamei, Saeed
منشور في: (2012) -
Design of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) engine nacelle / Asrul Azuwar Hashim
بواسطة: Hashim, Asrul Azuwar
منشور في: (2006)