ONERA M6 wing testcase Reynolds number -- CFD Online Discussion Forums

November 27, 2016, 10:23

ONERA M6 wing testcase Reynolds number

siw

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Stuart

Join Date: Jul 2009

Location: Portsmouth, England

Posts: 733

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Hi,

The ONERA M6 wing test case is at a Mach number of 0.8395 and Reynolds number of 11.72 million [Refs. 1 & 2]. How does this Reynolds number work out given the freestream static pressure and temperature in the weblinks? Have I made a silly mistake in my attached calc?

Ref. 1: http://www.grc.nasa.gov/WWW/wind/val...ng/m6wing.html
Ref. 2: http://www.grc.nasa.gov/WWW/wind/val.../m6wing01.html

Attached Files

ONERA M6 Wing.xlsx (10.0 KB, 5 views)

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