The Hong Kong Polytechnic UniversityDepartment of Aeronautical and Aviation Engineering

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Twelve ways to
make physics visible.

Shape a wing, follow the energy and change the response. Every experiment has adjustable inputs, linked visualisations and a saved A / live B comparison.

01 / Shape, propulsion & measurement

Aerodynamics & Fluid Mechanics

3D Wing Design & Downwash

Shape a wing. Watch the load move. Compare the induced-drag cost of carrying the same lift.

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Propulsion & Engine Systems

Turbofan Cycle & Bypass Ratio

Split the airflow between core and bypass. Trace the shaft work, nozzle states and two contributions to net thrust.

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Aircraft Systems

Pitot–Static & Airspeed

Separate true speed from pressure-derived indications. Trap a pressure, change the flight condition and reveal the measurement error.

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02 / Waves, rotating blades & braking

Aerodynamics & Fluid Mechanics

Oblique Shocks & Expansion Fans

Drag a compression or expansion corner. See the wave geometry and thermodynamic change emerge from the same solution.

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Propulsion & Engine Systems

Propeller Pitch & Efficiency

Change pitch and twist, then inspect the local incidence. Couple blade-element forces to the axial momentum of the slipstream.

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Aircraft Systems

Wheel Braking, Anti-skid & Brake Energy

Watch wheel speed separate from ground speed. Compare locked-wheel braking with a pressure-dumping anti-skid controller.

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03 / Balance, operating points & guidance

Flight Dynamics & Control

Payload, Fuel & Centre of Gravity

Drag the payload along the cabin and choose which tank empties first. Follow centre-of-gravity travel, tail force and elevator demand.

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Propulsion & Engine Systems

Compressor Map & Operating Limits

Move the corrected-speed line and the throttle characteristic. Locate the operating point and distinguish a map boundary from a surge prediction.

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Flight Dynamics & Control

Localiser & Glideslope Capture

Move the initial aircraft position. Watch lateral and vertical guidance capture a synthetic approach while wind changes the ground track.

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04 / Near-wall flow, asymmetry & cabin systems

Aerodynamics & Fluid Mechanics

Boundary Layer & Flow Separation

Explore a laminar boundary layer under a favourable or adverse pressure gradient. Move the probe and inspect the calculated velocity profile.

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Flight Dynamics & Control

Engine-out Asymmetry & Control

Reduce left-engine thrust and balance the yawing moment. Follow sideslip, yaw rate and the resulting attitude in a bounded lateral model.

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Aircraft Systems

Cabin Pressurisation & Thermal Control

Set the climb, change the supply and open a leak. Trace cabin pressure and temperature as a controller changes the outflow area.

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These are original teaching models with explicit limits. Open the model notes in each experiment to see which relationships are calculated and which assumptions are illustrative.