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.


Le Moigne [22]0.26970.0176315.29
Neilsen and Anderson [23]0.25300.0168015.06
Lee et al. [24]0.26220.0175114.97
Present computations0.27120.0161016.84