The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman
The topic of this final project is “The Analysis of SME MD3-160 Aircraft Wing Structure”. This analysis uses a real model of aircraft structure courtesy of the SME Aviation Sdn. Bhd. which is located at Subang, Selangor Darul Ehsan. This final project focuses more onto the structural analysis compar...
محفوظ في:
المؤلف الرئيسي: | Abdul Rahman, Wan Arma Idayu |
---|---|
التنسيق: | أطروحة |
اللغة: | English |
منشور في: |
2002
|
الموضوعات: | |
الوصول للمادة أونلاين: | https://ir.uitm.edu.my/id/eprint/21248/1/TD_WAN%20ARMA%20IDAYU%20ABDUL%20RAHMAN%20EM%2002_5.pdf |
الوسوم: |
إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
مواد مشابهة
-
Distributed collison avoidance algorithms for autonomous unmanned aircraft /
بواسطة: Albaker, Baraa Munqith Abdul Jabar
منشور في: (2012) -
Aircraft-lightning dynamics assessment using computer based simulations /
بواسطة: Sanmugasundaram, Thirukumaran -
Design of a composite morphing wing /
بواسطة: Wan Luqman Hakim Wan A. Hamid
منشور في: (2019) -
A novel high-precision ground-based aircraft landing system capitalizing on towers trilateration
بواسطة: Salih, Ahmad Abbas Al-Ameen
منشور في: (2013) -
Design of flapping mechanism and analysis on the lift force of the wings /
بواسطة: Saktishvikmend Anbalagan
منشور في: (2019)