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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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書誌詳細
主要な著者:	Othman, Nurain, Ishak, Iskandar Shah, Dahalan, Md. Nizam
フォーマット:	論文
言語:	English
出版事項:	Penerbit Akademia Baru 2022
主題:	TJ Mechanical engineering and machinery
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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