Computational fluid dynamics (CFD) analysis of UiTM blended-wing-body (BWB) baseline-n UAV with canard deflection of -5 degree at 0.1 Mach number / Nik Mohd Hanif Nik Ibrahim
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主要作者: | Nik Ibrahim, Nik Mohd Hanif |
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格式: | Thesis |
语言: | English |
出版: |
2010
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在线阅读: | https://ir.uitm.edu.my/id/eprint/68295/1/68295.pdf |
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