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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.
Here are the budgets of Brandon Surgery Center for the most recent historical quarter (in thousands of dollars): Static Flexible Actual Number of surgeries 1,200 1,300 1,
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Framework In the laboratory we will deal with low speed flows, at first using the potential flow solver. We will also investigate behaviour for the NACA 4-series of aerofoils.
Bearing stresses are very common in aerospace engineering. It occurs on the surface of contact between any two structural members. Bolts, pins, and rivets are classic examples of
Difference between Blow hole and pin hole porosity Blow hole : They appear as cavities in a casting. When they are visible on the upper surface of the castings, th
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Permeability of Moulding Sand is the property of the sand, which permits the gases and steam to escape through the sand mould. For this purpose, the sand must be porous. Permeabil
Static electricity in aircraft: As mentioned earlier, the effects of static electricity are of considerable importance in the design of aircraft and aircraft equipment. An air
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