File:CL, CD NACA632618.png
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Summary
| Description | English: Lift and drag coefficients for NACA 633618 airfoil. Red values at Re=9.10^6, blue at 3.10^6. Full curves Cl, dashed Cd. Data Nasa via Abbott & Doenhoff, Theory of wing sections. |
| Date | |
| Source | Own work |
| Author | TSRL |
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 16:38, 14 June 2012 | | 414 × 291 (15 KB) | TSRL |
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