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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Bibliographic Details
Main Authors: Othman, Nurain, Ishak, Iskandar Shah, Dahalan, Md. Nizam
Format: Article
Language:English
Published: Penerbit Akademia Baru 2022
Subjects:
Online Access: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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