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AC6-16: NASA Rotor 37 - transition modelling - total pressure ratio as a function of the mass flow rate.

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Software used	Matplotlib version3.8.3, https://matplotlib.org/
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Vertical resolution	39.37 dpc

Revision as of 13:45, 21 August 2024 (view source) Lionel.Temmerman (talk \| contribs) (AC6-16: NASA Rotor 37 - transition modelling - total pressure ratio as a function of the normalized mass flow rate.)		Latest revision as of 13:46, 21 August 2024 (view source) Lionel.Temmerman (talk \| contribs) (→‎Summary)
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	== Summary ==		== Summary ==
	AC6-16: NASA Rotor 37 - transition modelling - total pressure ratio as a function of the ~~normalized~~ mass flow rate.		AC6-16: NASA Rotor 37 - transition modelling - total pressure ratio as a function of the mass flow rate.