Consider an infinitely thin flat plate of chord c at an angle of attack α in asupersonic flow. The pressures on the upper and lower surfaces aredifferent but constant over each surface; that is, pu(s) = c1 andpl (s) = c2, where c1 and c2 are constants and c2 > c1. Ignoring the shearstress, calculate the location of the center of pressure.
Consider an infinitely thin flat plate of chord c at an angle of attack α in asupersonic flow. The pressures on the upper and lower surfaces aredifferent but constant over each surface; that is, pu(s) = c1 andpl (s) = c2, where c1 and c2 are constants and c2 > c1. Ignoring the shearstress, calculate the location of the center of pressure.
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 infinitely thin flat plate of chord c at an angle of attack α in a
supersonic flow. The pressures on the upper and lower surfaces are
different but constant over each surface; that is, pu(s) = c1 and
pl (s) = c2, where c1 and c2 are constants and c2 > c1. Ignoring the shear
stress, calculate the location of the center of pressure.
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