Govt. Exams
Entrance Exams
τ = μ(du/dy) = 0.1 × 50 = 5 Pa
Continuity equation for incompressible flow states Q = constant, so A₁v₁ = A₂v₂
Cd < 1 accounts for vena contracta and frictional losses in actual orifice flow compared to ideal flow.
Boundary layer develops due to viscous effects that cause velocity gradient near solid surfaces, creating shear stress.
Hagen-Poiseuille equation is valid for incompressible, fully developed laminar flow in circular pipes without entrance effects.
Kinematic viscosity ν = μ/ρ = 0.8/800 = 1.0 × 10⁻³ m²/s
From continuity equation A₁V₁ = A₂V₂, when area decreases, velocity must increase to maintain constant mass flow rate.
The dynamic viscosity of water at 20°C is approximately 1.002 × 10⁻³ N·s/m² or 0.001 N·s/m², which is used in Reynolds number calculations.
Bernoulli's equation is valid for inviscid (frictionless), incompressible, steady flow along a streamline. It represents energy conservation in such flows.
Pressure coefficient Cₚ = (P - P∞)/(0.5ρV∞²) is a dimensionless quantity used in aerodynamics and fluid mechanics.