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Consider an airfoil in a wind tunnel (i.e., a wing that spans the entire testsection). Prove that the lift per unit span can be obtained from the pressuredistributions on the top and bottom walls of the wind tunnel (i.e., from thepressure distributions on the walls above and below the airfoil).

Consider an airfoil in a wind tunnel (i.e., a wing that spans the entire testsection). Prove that the lift per unit span can be obtained from the pressuredistributions on the top and bottom walls of the wind tunnel (i.e., from thepressure distributions on the walls above and below the airfoil).

Elements Of Electromagnetics
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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Consider an airfoil in a wind tunnel (i.e., a wing that spans the entire test
section). Prove that the lift per unit span can be obtained from the pressure
distributions on the top and bottom walls of the wind tunnel (i.e., from the
pressure distributions on the walls above and below the airfoil).

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