The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
In line with the advancement of micro processor technology, availability small scale aircraft engine model, light weight material and also better understanding in the aircraft design process had brought a current attention to develop autonomous flying vehicles. This kind of vehicle has offered v...
محفوظ في:
| المؤلف الرئيسي: | |
|---|---|
| التنسيق: | أطروحة |
| اللغة: | English English English |
| منشور في: |
2011
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| الموضوعات: | |
| الوصول للمادة أونلاين: | http://eprints.uthm.edu.my/2583/1/24p%20AHMAD%20ESHTIWEY%20AL%20AIAN.pdf http://eprints.uthm.edu.my/2583/2/AHMAD%20ESHTIWEY%20AL%20AIAN%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/2583/3/AHMAD%20ESHTIWEY%20AL%20AIAN%20WATERMARK.pdf |
| الوسوم: |
إضافة وسم
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