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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.
design a connectivity diagram for a 7.3 m satellite antenna
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Is there anyone on your staff good with HEC-HMS software for modeling rain events?
Q. Explain briefly the Friction welding techniques. OR Discuss any two solid state welding methods.
Inner rooms - means of escape: I nner rooms are rooms from which the means of escape require people to travel through another room (called the access room). These are comm
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False Alarms & CM The mis-association of false alarms with target tracks has two main e!ects. - It tends to increase the actual tracking errors in the system because
Also called 1-bit DAC or sigma-delta DAC. It uses pulse-density modulation (PDM) which encodes the signal amplitude by the relative density of the pulses. The output voltage has on
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