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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.
Fire alarm systems: Fire alarm systems can be very complex and it is usually not possible for an enforcing officer to check all the cabling, the components, the software and t
name the functions of the CIPM
Ubiquitous network applications are generally designed for a whole network. This notion should be reflected in the way a network is programmed. We believe that providing abstractio
Assume that a movie is two hours long, that the frame rate is 30 frames per second, and that the resolution per frame is 1080i (1920×1080 pixels per frame), and that each pixel is
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The demand placed on a system is described by a lognormally distributed random variable with mean 50 and standard deviation of 10. The capacity of the system is modeled by a Weibul
application of newton rings.
explain the funcyions and structure of foreign exchange market.
Give two functions of dimensions.
USE OF MULTICYLINDER ENGINE If, in a multi cylinder engine, power strokes are staggered, the limitation of flywheel can be overcome to a large extent. Torque diagram for 2 cyli
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