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...

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Bibliographic Details
Main Author: Al Aian, Ahmad Eshtiwey
Format: Thesis
Language:English
English
English
Published: 2011
Subjects:
Online Access:http://eprints.uthm.edu.my/2583/1/24p%20AHMAD%20ESHTIWEY%20AL%20AIAN.pdf
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