Open Access
Table 7
Effect of T0 the zero lift angle for the third non-symmetric airfoil in function of M0.
| PG | HT T0 (K) | |||
|---|---|---|---|---|
| M0 | γ = 1.402 | 1000 | 2000 | 3000 |
| 2.00 | 1.12621 | 1.06831 | 1.00951 | 0.98844 |
| 3.00 | 1.22893 | 1.16998 | 1.10840 | 1.08275 |
| 4.00 | 1.36949 | 1.30556 | 1.21869 | 1.19970 |
| 5.00 | 1.44686 | 1.38326 | 1.26308 | 1.24281 |
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