Govt. Exams
Entrance Exams
For convergent nozzles, mass flow becomes independent of downstream pressure when throat reaches sonic conditions (M = 1)
Boundary layer separation occurs when an adverse (positive) pressure gradient opposes the flow, causing the flow to reverse near the wall and separate from the surface.
For a given pipe with constant diameter and same fluid (constant Re behavior), the friction factor depends on Re and relative roughness. For geometrically similar conditions, f remains relatively constant in turbulent flow.
In a converging-diverging nozzle for supersonic flow, sonic conditions (M=1) occur at the throat. Beyond the throat, the flow accelerates to supersonic speeds.
In turbulent flow, ΔP ∝ f × V^m where m is between 1.8-2 depending on friction factor variation. Not exactly V² due to changing friction factor with Re.