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SUPERSONIC INTAKES
At supersonic speeds, the pitot type of air intake is unsuitable due to the severity of shock waves which form and progressively reduce the intake efficiency as speed increases. To overcome this problem the compression intake was designed.
This type of intake produces a series of mild shock waves without reducing the intake efficiency, as the aircraft speed increases, so also does the intake compression ratio. At high mach numbers it becomes necessary to have an air intake which has a variable thrust area and spill doors to control the column of air.
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Noise reduction The problem of engine noise has always been associated with aircraft. Increases in engine power have given rise to increases in noise and the indications are t
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Noise Suppression in Aircraft Design: It has been seen that the first step towards noise suppression is at the design stage of the rotating and static parts of the engine. The
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