Journal of Aircraft
 2017
DOI: 10.2514/1.c033568
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Numerical Study of the Reliability of Wind-Tunnel Wall Corrections for Wingtip Flow

Antoine Joulain
1
,
Damien Desvigne
2
,
David Alfano
3
et al.

Abstract: McAlister and Takahashi [2] is investigated at an uncorrected chordbased Reynolds number Re = 1.6 × 10 6 , Mach number M = 0.131 and angle of attack α = 12 • .

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