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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2019
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Article
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Tab 4
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Research Article
Crosswise Wind Shear Represented as a Ramped Velocity Profile Impacting a Forward-Moving Aircraft
Table 4
Lift and drag coefficients of the ONERA M6 wing with and without folding tips.
Present computations
0.2712
0.01610
16.84
Plain ONERA M6 wing under SW1
0.3225
0.01712
18.83
ONERA M6 wing with folding tips
0.3773
0.01912
19.73