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Estimation of nonlinear surface pressure characteristics of aerofoil: A 0-1 test approach

We investigate the nonlinear behaviour of the surface flow over a two-dimensional NACA 2415 airfoil undergoing turbulent inflow having 8.46% TI at Re=3.01×105 using the 0-1 test for chaos. It clearly identifies the overall surface flow changes and also finds the transitions from regular to chaotic b...

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Váldodahkkit: S. Arunvinthan, R. Gopal, V. K. Chandrasekar, S. Nadaraja Pillai
Materiálatiipa: Artigo
Giella:Inglês
Almmustuhtton: AIP Publishing LLC 2019-05-01
Ráidu:AIP Advances
Liŋkkat:http://dx.doi.org/10.1063/1.5102154
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