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Steam Jet vaccum ejector


Posted by: seminar class
Created at: Saturday 12th of March 2011 05:23:25 AM
Last Edited Or Replied at :Tuesday 05th of April 2011 06:35:58 AM
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ssure energy of a motivating fluid to velocity energy to entrain suction fluid and then to recompress the mixed fluids by converting velocity energy back into pressure energy. This is based on the theory that a properly designed nozzle followed by a properly designed throat or venturi will economically make use of high pressure fluid to compress from a low pressure region to a higher pressure. This change from pressure head to velocity head is the basis of the jet vacuum principle.
The nozzle provides controlled expansion of the motive steam to convert pressure in to velocity which creates a ..................[:=> Show Contents <=:]



Vortex refrigeration


Posted by: summer project pal
Created at: Sunday 09th of January 2011 07:07:54 PM
Last Edited Or Replied at :Sunday 09th of January 2011 07:07:54 PM
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ffect of 336*1000kj/kg in 24 hours is rated as One TONNE,
In si units its conversions rounded off to 3.5kj/s(kw) or 210 kj/min.
CHAPTERII
Vortex


Vortex created by the passage of an aircraft wing, revealed by colored smoke.
A vortex is a spinning, often turbulent, flow of fluid. Any spiral motion with closed streamlines is vortex flow. The motion of the fluid swirling rapidly around a center is called a vortex. The speed and rate of rotation of the fluid are greatest at the center, and decrease progressively with distance from the center.

1.1 Properties of vortex
Vortices..................[:=> Show Contents <=:]



TURBOFAN ENGINES


Posted by: summer project pal
Created at: Saturday 08th of January 2011 12:40:23 PM
Last Edited Or Replied at :Tuesday 26th of April 2011 05:58:55 AM
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9.81 m / s 2

= 9.941 * 457.2

Thrust = 4545.025 kg.

If the pressure at the exit plane is not the same as the atmospheric pressure and the aircraft were not standing still, the formula would be somewhat different.
It is not very practical to try to compare jet engine output in terms of horsepower. As a rule of thumb, however, it may be noted that that at 375 miles per hour (mph), one pound of thrust equals one horsepower, at 750 mph one pound of thrust equals two horsepower.

Thrust Equation for Turbojet-Type Engines
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