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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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e predicted results of the cylinder pressure and rate of heat release and the measured data , and showed that the predictions agreed well with the measured data.

Introduction

-The thermodynamic cycle analysis and the performance prediction of diesel engines using the engine cycle simulation programs has become an established part of the diesel engine research and development.
-Particularly ,the engine simulation programs based on the single-zone combustion model are widely used by most engine manufacturers because of simplicity and low operating cost in spite of their sh..................[:=> Show Contents <=:]



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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e studied the expansion ratio and compression ratio through performance calculation (6), paying attention to the pulsation inside the inlet and exhaust pipes, and grasped the appropriate values. Fig. 1 shows the relation between expansion ratio and estimated thermal efficiency, indicating obviously that the engine thermal efficiency of 40% can be achieved by setting the expansion ratio (compression ratio based on bottom dead center) to 15. Thus, the expansion ratio based on the calculation result was set to 15. Further, the inlet valve close timing was experimentally set. Fig. 2 shows the rela..................[:=> 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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uch greater. Although colloid thrusters have been around almost as long as ion engines they have not been developed to flight status. In the laboratory they typically have specific impulses around 1,000 sec.
FIGURE 3.7. SINGLE COLLOID THRUSTER EMITTER
Many of these would be tied together to create a single large thruster.
3.3. Electromagnetic Rocket Engines
This is by far the largest group of electric thrusters with many different techniques used to create thrust. As widely divergent as these thrusters may seem they all use the same principle: the Lorenz force.
If you have an electric cur..................[:=> 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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ne of two alternative stable states. This is achieved by using the Coanda effect of jet
attachment to walls. There are two attachment walls, W1 and W2 (Fig. 2) placed
symmetrically on both sides of the path of the main jet, which is formed by the supply
flow issuing from the supply nozzle. The jet may attach equally well to either one of the
two walls, which keep it deflected and guide it into one of the two collectors, connected
to the output terminals Y1 and Y2. Shown in Fig. 3 there are computed pathlines in the
valve for the state with the jet guided into the output terminal Y2. The ..................[:=> 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..................[:=> 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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..................[:=> 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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ns, 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 operates at leaner fuel levels, nitrogen emissions increase. Therefore, for lean burn engines to replace traditional fuel mixture engines, nitrogen oxide emission must be reduced. T..................[:=> 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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ston engines and jet engines, their primary difference due to the different ways of controlling the engines.

Electronics' superior accuracy led to early generation analogue electronic control first used in Concorde's Rolls-Royce Olympus 593 in the 1960s. Later in the 1970s NASA and Pratt and Whitney experimented with the first experimental FADEC, first flown on an F-111 fitted with a highly modified Pratt & Whitney TF-30 left engine. The experiments led to Pratt & Whitney F100 and Pratt & Whitney PW2000 being the first military and civil engines respectively fitted with FADEC and later the ..................[:=> Show Contents <=:]



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