Calculate the total drag on an airfoil that has a chord length of 2 m and a

Question:

Calculate the total drag on an airfoil that has a chord length of 2 m and a span of 10 m. The airfoil is at 3000 m flying at

(a) 600 km/h

(b) 150 km/h. Use Fig. 17.11 for C D and a = 15°.

Cz]CD FÖFD 2.00 t0.40 CD -35 Stall point a =19.6 + 1.50+0.30+F30 -FFD -25 1.00+0.20+20 15 0.50+0.10+ 10 0+0 -5 20 10 15

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Applied Fluid Mechanics

ISBN: 978-0132558921

7th edition

Authors: Robert L. Mott, Joseph A. Untener

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Question Posted: Jan 10, 2019 09:13 AM

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Calculate the total drag on an airfoil that has a chord length of 2 m and a

Question:

Cz]CD FÖFD 2.00 t0.40 CD -35 Stall point a =19.6 + 1.50+0.30+F30 -FFD -25 1.00+0.20+20 15 0.50+0.10+ 10 0+0 -5 20 10 15 25 30 Angle of attack, a (deg)

Step by Step Answer:

a b v 150 10 3 3600 41...View the full answer

Applied Fluid Mechanics

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