Experimental result analysis for scaled model of UiTM tailless blended wing-body (BWB) Baseline 7 unmanned aerial vehicle (UAV)
Blended wing-body (BWB) aircraft having planform configuration similar to those previously researched and published by other researchers does not guarantee that an efficient aerodynamics in term of lift-to-drag ratio can be achieved. In this wind tunnel experimental study, BWB half model is used. Th...
Main Authors: | Ahmad, A.M (Author), Kuntjoro, W. (Author), Latif, Z.A.A (Author), Nasir, R.E.M (Author), Romli F.I (Author), Saad, R.M (Author) |
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Format: | Article |
Language: | English |
Published: |
Institute of Physics Publishing
2017
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Subjects: | |
Online Access: | View Fulltext in Publisher View in Scopus |
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