File:AC6-16-pr vs qm scheme.png

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AC6-16-pr_vs_qm_scheme.png ‎(640 × 480 pixels, file size: 48 KB, MIME type: image/png)

Summary

AC6-16 - NASA Rotor 37 - total pressure ratio as a function of the mass flow rate (kg/s) - effect of the numerical scheme - Cadence

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current09:55, 8 August 2024Thumbnail for version as of 09:55, 8 August 2024640 × 480 (48 KB)Lionel.Temmerman (talk | contribs)AC6-16 - NASA Rotor 37 - total pressure ratio as a function of the mass flow rate (kg/s) - effect of the numerical scheme - Cadence

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