Consider a stationary, thin, flat plate with area of 2.00 m^2 for each face oriented perpendicular to a flow. The pressure exerted on the front face of the plate (facing into the flow) is 1.32 atm , and is constant over the face. The pressure exerted on the back face of the plate (facing away from the flow) is 2,088.6 lb/ft^2 and is constant over the face. Calculate the aerodynamic force in kilo-newtons on the plate.
Consider a stationary, thin, flat plate with area of 2.00 m^2 for each face oriented perpendicular to a flow. The pressure exerted on the front face of the plate (facing into the flow) is 1.32 atm , and is constant over the face. The pressure exerted on the back face of the plate (facing away from the flow) is 2,088.6 lb/ft^2 and is constant over the face. Calculate the aerodynamic force in kilo-newtons on the plate.
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 5.20P
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