Wind tunnels cover facilities and associated instrumentation used to simulate aerodynamic airflow conditions over aircraft structures, aerofoils, control surfaces, and scale models, encompassing subsonic, transonic, supersonic, and hypersonic test regimes, with integrated pressure tapping arrays, pitot-static probes, hot-wire anemometry, PIV (Particle Image Velocimetry), and force-balance systems to characterise lift, drag, and boundary-layer behaviour.
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