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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.

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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Fp p dA Usurface Wake Fig. 9.9 Flow over a flat plate normal to the flow Drag coefficients are usually obtained empirically 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.
Transcribed Image Text:Fp p dA Usurface Wake Fig. 9.9 Flow over a flat plate normal to the flow Drag coefficients are usually obtained empirically 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.
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