Question: Need help with this problem Consider a at plate at- zero angle of attack in a hypersonic flow at Mach 10 at standard sea level

Need help with this problem

Consider a at plate at- zero angle of attack in a hypersonic flow at Mach 10 at standard sea level conditions. At. a point. (1.5 m downstream from the leading edge, the local shear stress at the wall is 282 hat/mg. The gas temperature at the wall is equal to standard sea level temperature. At this point. calculate the velocity gradient at the wall normal to the wall

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