CFD study on NACA 4415 airfoil implementing spherical and sinusoidal Tubercle Leading Edge

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Finite Element Modeling for the Simulation of the Quasi-Static Compression of Corrugated Tapered Tubes
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Finite Element Modeling for the Simulation of the Quasi-Static Compression of Corrugated Tapered Tubes

Published on: January 6, 2023

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S M A Aftab1, K A Ahmad1,2

  • 1Dept of Aerospace Engineering, Universiti Putra Malaysia, Selangor, 43400, Malaysia.

Plos One
|August 30, 2017
PubMed

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