Static analysis of unsteady aerodynamics wake of simplified helicopter model via simulation work
Computational tools have led and helped researchers in providing advanced results, notably in rotorcraft research, as flow around the helicopter is dominated by complex aerodynamics and flow interaction phenomena. This research work aimed to evaluate the aerodynamic computational results on a simpli...
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主要な著者: | Othman, Nurain, Ishak, Iskandar Shah, Dahalan, Md. Nizam |
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フォーマット: | 論文 |
言語: | English |
出版事項: |
Penerbit Akademia Baru
2022
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主題: | |
オンライン・アクセス: | http://eprints.utm.my/id/eprint/98479/1/NurainOthman2022_StaticAnalysisofUnsteadyAerodynamics.pdf http://eprints.utm.my/id/eprint/98479/ http://dx.doi.org/10.37934/arfmts.89.1.142153 |
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