2- For two-dimensional laminar jet flow, simplify the boundary layer equation and obtain relationship for p...

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2- For two-dimensional laminar jet flow, simplify the boundary layer equation and obtain relationship for p and q using the following stream function. 3- For flow with velocity profile: U(x)= 1.0+2.0 X UL = 106, it is desirable: A) separation point (x/L) lam-sep b) Instabili V For the case where point (x/L)cr using Wazzan method 4- For the following approximate velocity profile that is used for the bounda surface, using the Von Krmn integral equation of the boundary layer for zero pressure layer on calculate the shape factor (H) and the value of the following functions and compare wit corresponding to the Blasius boundary layer (from the book). (6/x)Re/2, (6*/x)Re/2, (0/x)Rel/ 1/2 U (y) Ue D S 0 = 8 ( 11 ) fio = 2 - (1) for y 8) 2- For two-dimensional laminar jet flow, simplify the boundary layer equation and obtain relationship for p and q using the following stream function. 3- For flow with velocity profile: U(x)= 1.0+2.0 X UL = 106, it is desirable: A) separation point (x/L) lam-sep b) Instabili V For the case where point (x/L)cr using Wazzan method 4- For the following approximate velocity profile that is used for the bounda surface, using the Von Krmn integral equation of the boundary layer for zero pressure layer on calculate the shape factor (H) and the value of the following functions and compare wit corresponding to the Blasius boundary layer (from the book). (6/x)Re/2, (6*/x)Re/2, (0/x)Rel/ 1/2 U (y) Ue D S 0 = 8 ( 11 ) fio = 2 - (1) for y 8)

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