Research Article

Crosswise Wind Shear Represented as a Ramped Velocity Profile Impacting a Forward-Moving Aircraft

Table 2

Lift and drag coefficients with and without folding tips.

BGK 3D plain wingBGK 3D wing with folding tip

No shear0.62990.0380416.4040.71330.038918.337
SW10.64780.0350118.5030.88910.0245836.172
SW20.59180.0389915.1780.72630.0393118.48