Course notes – these are essential and required.

Munson, B.R., Young, D.F., Okiishi, T.H., Fundamentals of Fluid Mechanics, John Wiley and Sons Inc, Any Edition.

John D. Anderson, “Modern Compressible Flow with Historical Perspective”, 3rd Edition, Mc Graw-Hill, 2003.

Lectures supported by problem-solving tutorials developing material covered in lectures

The required time commitment from the beginning of semester to the end of the final exam is 48 hours attendance at lectures and tutorials, 48 hours of self directed learning, 3 hours of laboratory work, 40 hours completing assignments and laboratory reports and 40 hours of revising course material and preparing for the exam.

• fully developed flow;
• losses and flow behaviour in pipes, ducts, pipe fittings;
• pipe systems and networks;
• flow meters
• calculation of energy loss, flow rates, pipe sizes etc;
• matching of flow systems to turbomachines.

• Behaviour and theory of boundary layers
• Laminar and turbulent boundary layers
• Von-Karman momentum integral equation
• Effect of pressure gradient

• aerodynamic forces on streamlined and bluff bodies;
• flow separation;
• lift and drag on wings, including induced drag;
• theory of lift and circulation;
• vortex shedding.

• Drag and road load
• Vortex structure
• Shape optimisation

• Isentropic Processes of Ideal Gases (Review)
• Stagnation or Total Properties
• 1-Dimensional Isentropic Wave theory
• Mach Waves
• Shock Waves

• Isothermal-Isentropic Flow
• Isoenergetic, Isentropic Flow of an Ideal Gas
• Mass Flow Relations and Choking
• Flow in a Converging Nozzle
• Convergent-Divergent Supersonic Diffusers
• 1-DFrictional Flow in a Duct (Fanno flow)
• 1-D Flow with Heat Addition Rayleigh flow)
• Aircraft intake systems

• Compression and Expansion Waves
• External Flow Patterns
• Lift and Drag
• Linearised theory & compressibility corrections
• Critical Mach number
• Aerofoils in Transonic & Supersonic Flow
• Design Considerations

• Oblique shock waves – wedge flow
• Oblique shock waves – conical flow
• Expansion waves
• Calculation procedures
• Ackeret theory

• Boundary layer structure
• Effects of Mach number and Reynolds number
• Aerodynamic heating

• Schlieren, Shadowgraph & Interferometry
• Flow Facilities - Wind Tunnels & Shock-Tube Tunnels

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Assignments

All assignments are based on a problem-solving format. In each case a practical problem will be presented and the students will be asked to provide a solution to that problem. The problem format and difficulty are the same as the final exam. Each student’s submission will be assessed primarily on the quality of their approach to the problem. Students are required to state all assumptions used in their solutions, provide appropriate diagrams, and to follow a standard presentation procedure known as the “problem solving protocol”. Approximately 10% of the marks of each problem are awarded for fulfilling these requirements.

Laboratory

This laboratory consists of two parts. The first part is an experimental investigation of the pressure distribution over a wing using a wind tunnel. Students will be required to measure the pressure distribution and use the measured data to calculate the lift and pressure drag on the wing. The second part is an experimental investigation of a friction in pipe flows. The students will collect experimental data to analyse the impact of pipe diameter and velocity on head loss and to confirm the head loss predicted by a pipe friction equation associated with the flow of water through a smooth bore pipe. Students are required to submit group reports for each laboratory. Students must have submitted both reports and scored at least 35% overall to be eligible to pass the course. Further details are provided by the laboratory demonstrators.

Individual assignments are to be submitted by each student to myuni. Submitted assignments must be accompanied by an assessment cover sheet. Late assignments will be penalised 10% per day. Extensions for assignments will only be given in exceptional circumstances and a case for this with supporting documentation can be made in writing after a lecture or via email to the lecturer. Assignments will be assessed and returned within 3 weeks of the due date, along with a “model” solution prepared by the lecturer. There will be no opportunities for re-submission of work of unacceptable standard. Due to the large size of the class, feedback on assignments will be provided by comments on the returned assignments and general feedback given during the lectures and tutorials and on myuni.