A wing has an elliptical load distribution across its wingspan that totals a lift of2,500.0 N. Determine the induced drag of the wing in N. Round your answer to thefirst decimal place. The wing's aspect ratio is AR = 13.0 and the wing lift coefficient isCL = 0.80.Hint: This problem is solvable without density.

Given DataCL=0.8Total Lift (L)=2500NA.R=11

A wing has an elliptical load distribution across its wingspan that totals a lift of 2,500.0 N. Determine the induced drag of the wing in N. Round your answer to the fırst decimal place. The wing's aspect ratio is AR = 13.0 and the wing lift coefficient is CL = 0.80. %3D

A wing has an elliptical load distribution across its wingspan that totals a lift of 2,500.0 N. Determine the induced drag of the wing in N. Round your answer to the fırst decimal place. The wing's aspect ratio is AR = 13.0 and the wing lift coefficient is CL = 0.80. %3D

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Question

A wing has an elliptical load distribution across its wingspan that totals a lift of
2,500.0 N. Determine the induced drag of the wing in N. Round your answer to the
first decimal place. The wing's aspect ratio is AR = 13.0 and the wing lift coefficient is
CL = 0.80.
Hint: This problem is solvable without density.

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