Consider a wing with a linear AR of 8.0 and a taper of 0.5, the wing has a wingspan of 196 ft and a thin profile, a CL max of 1.6, estimate the maximum lift coefficient of the wing and the position in the chord of the profile when it enters in loss. Consider an arrow angle (1/4 of the chord) of 30 °

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Consider a wing with a linear AR of
8.0 and a taper of 0.5, the wing has a
wingspan of 196 ft and a thin profile, a
CL max of 1.6, estimate the maximum
lift coefficient of the wing and the
position in the chord of the profile
when it enters in loss.
Consider an arrow angle (1/4 of the
chord) of 30 °
Transcribed Image Text:Consider a wing with a linear AR of 8.0 and a taper of 0.5, the wing has a wingspan of 196 ft and a thin profile, a CL max of 1.6, estimate the maximum lift coefficient of the wing and the position in the chord of the profile when it enters in loss. Consider an arrow angle (1/4 of the chord) of 30 °
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