Fluid Mechanics II
Differential analysis and the Navier-Stokes equations, dimensional analysis and model testing, potential flow, laminar and turbulent boundary layers, drag and lift, compressible flow in nozzles and shocks, and the theory of pumps, turbines and fans, applied to a water utility's intake, pumping, air-valve and wind turbine projects in Regina.
MEC-370 Year 3 3 credits 12 lessons · 5 h 16 min ▶ Video lessons coming soon
Offered by HSM University · Mechanical Engineering
This is the Canadian version of this course. See the American version.
What you'll learn
- Derive the differential continuity and Navier-Stokes equations for a Newtonian fluid, state their boundary conditions, and solve Couette, Poiseuille and falling-film flows, checking that the laminar assumption holds.
- Form dimensionless groups with the Buckingham Pi theorem, interpret the Reynolds, Froude, Mach and other named numbers, and scale model tests of pumps and intakes to prototypes, including efficiency step-up and scale effects.
- Build irrotational flows by superposing uniform flow, sources, sinks, vortices and doublets, and use them to estimate intake capture zones, surface pressures and lift from circulation.
- Calculate laminar boundary-layer thickness, displacement and momentum thicknesses and skin friction from the Blasius solution and the momentum-integral method, and explain how pressure gradients cause separation.
- Predict transition, turbulent boundary-layer growth and friction drag on smooth and rough surfaces, apply the law of the wall, and design diffusers that avoid separation.
- Estimate drag on bluff and streamlined bodies across the range of Reynolds numbers, including settling velocities, the drag crisis, wind loads and vortex-induced vibration.
- Explain lift through circulation and the Kutta condition, apply thin-airfoil and lifting-line theory, and analyse the velocities and forces on a wind turbine blade section.
- Determine when gas flows are compressible, calculate the speed of sound in gases, liquids and pipes, and use Mach number and stagnation property relations.
- Analyse isentropic flow in converging and converging-diverging nozzles, identify choked flow, and size orifices for air valves, relief devices and leaks.
- Apply normal and oblique shock relations, locate shocks in nozzles, and evaluate the stored energy and hazards of compressed gases.
- Apply Euler's turbomachine equation and velocity triangles to centrifugal pumps, use specific speed and the affinity laws, and evaluate NPSH margins and suction specific speed.
- Select turbines, fans and pumps by specific speed, apply the fan laws and the Betz limit, and compare control methods for a pumping system over a year of operation.
Course content
12 lessons · 5 h 16 min total · final exam
- 1 Differential analysis and the Navier-Stokes equations 31 min · quiz
- 2 Dimensional analysis and similitude 26 min · quiz
- 3 Potential flow and superposition 26 min · quiz
- 4 Laminar boundary layers 26 min · quiz
- 5 Turbulent boundary layers, transition and separation 22 min · quiz
- 6 Drag on bluff and streamlined bodies 27 min · quiz
- 7 Lift, airfoils and finite wings 26 min · quiz
- 8 Compressible flow fundamentals 22 min · quiz
- 9 Isentropic flow in nozzles 28 min · quiz
- 10 Normal and oblique shocks 27 min · quiz
- 11 Pumps: Euler's equation, specific speed and cavitation 27 min · quiz
- 12 Turbines, fans and system matching: the capstone 28 min · quiz
- E Final exam 20 questions
Requirements
Recommended background. You can start any course at any time.
Description
Differential analysis and the Navier-Stokes equations, dimensional analysis and model testing, potential flow, laminar and turbulent boundary layers, drag and lift, compressible flow in nozzles and shocks, and the theory of pumps, turbines and fans, applied to a water utility's intake, pumping, air-valve and wind turbine projects in Regina.
Part of the Engineering stream, typically taken in year 3.