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M-COMBUSTION CHAMBER AND COLD STARTING OF CI ENGIINES


Posted by: seminar surveyer
Created at: Friday 08th of October 2010 03:27:26 AM
Last Edited Or Replied at :Friday 08th of October 2010 03:27:26 AM
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High Efficiency Miller Cycle Gas Engine full report


Posted by: project report tiger
Created at: Tuesday 16th of February 2010 09:43:19 AM
Last Edited Or Replied at :Tuesday 12th of October 2010 02:44:54 AM
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tically reduced.
Accordingly, higher boost pressure is required to maintain the same output, i.e., a turbocharger with low flow rate and high-pressure ratio is needed. However, among the turbochargers of mass production, there was no turbocharger like a Miller cycle engine with low flow rate and high-pressure ratio in addition to high efficiency. A turbocharger with low efficiency causes the exhaust pressure to rise and thereby the pump loss to increase, no matter how high the engine cylinder cycle efficiency is. The thermal efficiency consequently does not improve. In other words, a high eff..................[:=> Show Contents <=:]



chemical rocket engine full report


Posted by: project report tiger
Created at: Tuesday 16th of February 2010 09:22:03 AM
Last Edited Or Replied at :Tuesday 16th of February 2010 09:22:03 AM
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sual fuel of choice) is spring loaded against two stops near the exit of the thruster. When it's desired to fire it, an energy storage unit discharges an arc across the face of the propellant, ablating a small amount of the Teflon bar. Just like the rail gun and Magnetoplasmadynamic thruster, the current flowing through the vaporized propellant ionizes it and reacts with the magnetic field created by the current to accelerate the propellant out of the engine, creating thrust. As the propellant bar is eroded, the spring pushes it forward for the next pulse.
These engines are extremely simple,..................[:=> Show Contents <=:]



NO-MOVING-PART HYBRID-SYNTHETIC JET ACTUATOR full report


Posted by: project report tiger
Created at: Sunday 14th of February 2010 08:07:42 PM
Last Edited Or Replied at :Sunday 14th of February 2010 08:07:42 PM
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zzle width and w is the supply nozzle bulk exit velocity). The value is
plotted in Fig. 14 (for the data from Fig. 13) as a function of the supply nozzle Reynolds
number. Somewhat disappointingly, this non-dimensionalisation did not lead to a simple
overall picture.
Fig. 13. The frequency vs. loop length dependences obtained with the 10 mm dia loop tube at different
supply flow rates. The power law fit exponent near to 1.0 suggest that the frequency is simply inversely
proportional to the feedback loop length l.
Fig. 14. The experimental results obtained with the 10 mm dia loop tube at ..................[:=> Show Contents <=:]



smartcombustor


Posted by: vinayaka
Created at: Monday 08th of February 2010 11:01:00 PM
Last Edited Or Replied at :Wednesday 10th of February 2010 12:04:38 AM
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sir, will you please give me in..................[:=> Show Contents <=:]



ppt on rocket engine and their propelants


Posted by: l.chandrikarani
Created at: Saturday 02nd of January 2010 11:23:42 AM
Last Edited Or Replied at :Thursday 16th of February 2012 07:41:10 AM
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send this ppt about rocket engine&t..................[:=> Show Contents <=:]



Lean Burn Spark Ignition Engine


Posted by: computer science crazy
Created at: Tuesday 07th of April 2009 10:56:31 AM
Last Edited Or Replied at :Thursday 22nd of August 2013 12:23:44 AM
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engine -Lean Burn Spark Ignition Engine. The ratio of air to fuel in a spark ignition engine is on average 14.7:1. With the diminishing oil reserves and tightened legislations, fuel consumption and exhaust emission of spark ignition engines is to be reduced. The efficiency of lean burn engines is high due to the usage of higher air fuel ratio. Lean burn engine can reach unburned hydrocarbon and carbon monoxide emission targets. The design features of lean burn engines can be improved with increased compression ratio, mixture swirl, mixture preparation, and improved ignition. As engine operate..................[:=> Show Contents <=:]



FADEC - Full Authority Digital Engine Control


Posted by: computer science crazy
Created at: Saturday 20th of September 2008 12:15:06 PM
Last Edited Or Replied at :Saturday 20th of September 2008 12:15:06 PM
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e sensors. Apart from the key parameters that are monitored for a safe thrust control (shaft rotational speeds, pressures and temperatures at various points along the gas path) the FADEC also monitors hundreds of variou..................[:=> Show Contents <=:]



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