Research Article
Crosswise Wind Shear Represented as a Ramped Velocity Profile Impacting a Forward-Moving Aircraft
Table 3
Lift and drag coefficients on the ONERA M6 plain wing.
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| Le Moigne [22] | 0.2697 | 0.01763 | 15.29 | Neilsen and Anderson [23] | 0.2530 | 0.01680 | 15.06 | Lee et al. [24] | 0.2622 | 0.01751 | 14.97 | Present computations | 0.2712 | 0.01610 | 16.84 |
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