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.

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter5: Analysis Of Convection Heat Transfer

Section: Chapter Questions

Problem 5.3P: Evaluate the Nusselt number for flow over a sphere for the following conditions: D=0.15m,k=0.2W/mK,...

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