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A wind tunnel diagram which shows a fan drawing air past a model aircraft. [2] The measurements taken from models are applicable to full-size objects. The effect of streamlining is made visible in a wind tunnel. Shaping the body to make it more streamlined reduces fuel consumption.
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Name Status Size (W x H x L) Use Country Comments A2 Wind Tunnel [1]: 4 m × 94 m × 18 m (14 ft × 310 ft × 58 ft) Full scale general purpose
When a model is mounted on a wind tunnel balance attached to a sting, care must be taken that no parts of the model touch the sting during a wind tunnel test; the only support of the model must be through the balance. A CAD model of a monolithic internal six-component wind tunnel balance.
The power required to run a supersonic wind tunnel is enormous, of the order of 50 MW per square meter of test section cross-sectional area. For this reason most wind tunnels operate intermittently using energy stored in high-pressure tanks.
Transonic wind tunnels, between Mach 0.75 and Mach 1.2 (920 and 1,500 km/h; 570 and 910 mph; 260 and 410 m/s), are designed on similar principles as subsonic tunnels but present additional challenges, primarily due to the reflection of shock waves from the walls of the test section.