QUESTION 10 Choose all that are correct attributes of 3D wings a. Increased Aspect Ratio increases the induced drag b. The ideal spanwise lift distribution is elliptical C. The CL,Tip=O U d. Wings have a shallower lift-curve slope than aerofoils e. The ideal shap is elliptical f. Are infitnie 8. Increased Aspect Ratio increases tip votex strength Oh. The CL.root=0 i. Wings produce more induced drag than aerofoils UJ. Wings produce less parasite drag than aerofoils

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QUESTION 10
Choose all that are correct attributes of 3D wings
a. Increased Aspect Ratio increases the induced drag
b. The ideal spanwise lift distribution is elliptical
OC. The CL,Tip =0
Ud. Wings have a shallower lift-curve slope than aerofoils
e. The ideal shap is elliptical
f. Are infitnie
8. Increased Aspect Ratio increases tip votex strength
Oh. The CL.root =0
i.
Wings produce more induced drag than aerofoils
UJ. Wings produce less parasite drag than aerofoils
Transcribed Image Text:QUESTION 10 Choose all that are correct attributes of 3D wings a. Increased Aspect Ratio increases the induced drag b. The ideal spanwise lift distribution is elliptical OC. The CL,Tip =0 Ud. Wings have a shallower lift-curve slope than aerofoils e. The ideal shap is elliptical f. Are infitnie 8. Increased Aspect Ratio increases tip votex strength Oh. The CL.root =0 i. Wings produce more induced drag than aerofoils UJ. Wings produce less parasite drag than aerofoils
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