1. A two dimensional supersonic airfoil has the cross-section shown below (base: 2.8 m, base angles 10). Its base (chord) is parallel to a flow M 2.4 at an atmospheric pressure of 25kPa. Find the lift and drag forces (normal and parallel to flow) per unit span. Hint: these forces are the result of the pressures acting on the airfoil M-2.4 T.4m 1.4m

1. A two dimensional supersonic airfoil has the cross-section shown below (base: 2.8 m, base angles 10). Its base (chord) is parallel to a flow M 2.4 at an atmospheric pressure of 25kPa. Find the lift and drag forces (normal and parallel to flow) per unit span. Hint: these forces are the result of the pressures acting on the airfoil M-2.4 T.4m 1.4m

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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