Consider a finite wing with an aspect ratio of 5. Assume an elliptical lift distribution. The lift slope for the airfoil section is0.1/degree.Calculate the lift slope (in 1/rad) for a swept wing, with a half-chord line sweep of 45 degrees. (Round the final answer to three decimalplaces.)The lift slope isper radian.

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Consideld mite wIng with dll aspect Iadtio dil elliptiIcal mt distibution1. me mt Slope foI Lhe alnoll sectioT 0.1/degree. Calculate the lift slope (in 1/rad) for a swept wing, with a half-chord line sweep of 45 degrees. (Round the final answer to three decimal places.) The lift slope is iper radian.

Consideld mite wIng with dll aspect Iadtio dil elliptiIcal mt distibution1. me mt Slope foI Lhe alnoll sectioT 0.1/degree. Calculate the lift slope (in 1/rad) for a swept wing, with a half-chord line sweep of 45 degrees. (Round the final answer to three decimal places.) The lift slope is iper radian.

International Edition---engineering Mechanics: Statics, 4th Edition

4th Edition

ISBN:9781305501607

Author:Andrew Pytel And Jaan Kiusalaas

Publisher:Andrew Pytel And Jaan Kiusalaas

Chapter9: Moments And Products Of Inertia Of Areas

Section: Chapter Questions

Problem 9.15P: Compute Ix and Iy for the W867 shape dimensioned in the figure. Assume that the section is composed...

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