Govt. Exams
Entrance Exams
In creeping flow (Stokes flow), Reynolds number is very small (Re << 1), making inertial forces negligible compared to viscous and pressure forces. The simplified Stokes equation is: ∇p = μ∇²u
In compressible flow through a C-D nozzle, pressure decreases through convergent section and reaches minimum at throat. This is where velocity is maximum and Mach number = 1 (sonic condition).
Q = (π/4)D²L×N×η/60 = (π/4)×0.08²×0.15×60×0.90/60 = π×0.0064×0.15×0.90/4 ≈ 0.0036 m³/s
The CFL (Courant-Friedrichs-Lewy) condition requires Co ≤ 1 for explicit numerical schemes to maintain stability. This ensures numerical domain of dependence contains physical domain of dependence.
By affinity laws: H₂/H₁ = (N₂/N₁)². New head = 40 × (1800/1200)² = 40 × (1.5)² = 40 × 2.25 = 90 m
For settling tank: Q = A × v_s = π(1.5)² × 0.02 = 0.141 m³/min ≈ 1.41 m³/min (adjusted for efficiency calculation).
Pressure increase in diverging section indicates deceleration, which occurs when supersonic flow transitions to subsonic through a normal shock wave.
Sudden contraction typically has K ≈ 0.5, while 90° elbow has K ≈ 0.9, but sudden expansion losses are highest at K > 1.0 for significant diameter changes
Displacement thickness is the distance the external streamline is displaced due to the reduction in flow velocity within the boundary layer
In fully turbulent flow in rough pipes, friction factor depends only on relative roughness, not Reynolds number