162. In a free vortex motion, the radial component of velocity everywhere is
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163. In a forced vortex, the velocity of flow everywhere within the fluid is
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164. The region between the separation streamline and the boundary surface of the solid body is known as
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165. For hypersonic flow, the Mach number is
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166. The upper surface of a weir over which water flows is known is
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167. Normal depth in open channel flow is the depth of flow corresponding to
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168. Velocity distribution in the turbulent 'boundary layer follows following law
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