Investigations relating to factors influencing the effectiveness of an aero-engine intake thermal anti-icing system
Thermal anti-icing systems are commonly used to protect aircraft leading edges from a potentially hazardous build-up of ice. Such systems have proven reliable in service and are relatively cheap and efficient. Typically, hot air is tapped from the engine compressor and ducted (via a regulation and c...
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| Format: | Default Thesis |
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1991
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| Online Access: | https://hdl.handle.net/2134/7201 |
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