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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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 09:55, 8 August 2024 | ![]() | 640 × 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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