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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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tion function and the white house-way’s heat release model were studied and successfully employed to the combustion simulation
- A comparison has been made between the 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 ..................[:=> 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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ormance specifications for this engine as well as for the series
of engines planned in the future.
2. ELEMENTARY TECHNOLOGY
This section deals with the applied elementary technologies and developments
2.1. Application of Miller cycle
The theoretical cycle efficiency in a conventional cycle internal combustion engine with nearly equivalent compression ratio and expansion ratio is expressed by equation (1).
Theory=1-1 - (1) where: engine compression ratio ( expansion ratio)
: Adiabatic index of working fluid
This indicates that it is necessary to increase the compression ratio in orde..................[:=> 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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emical systems. Third, thermal rejection systems for the engine and power conditioning unit (needed to convert the power from the power system into a flavor that the thruster prefers) can drive the weight of such a system beyond the practical limit.
5. CONCLUSION
Hardly a year goes by in the electric propulsion world without someone thinking up a new concept. These are always variations of the thrusters outlined in this page and attempt to get around one problem or another through an innovative geometry, ionization scheme, or other concept. It would be impossible to chronicle all of them but..................[:=> 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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The flow through the output
terminal Y1 is now negative and it should be noted that its magnitude is due to additional
jet-pumping effect of the control flow ” larger than the value given by Eq. (3). Subsequent further increase of the control flow rate brings no qualitative changes. The jet
pumping effect is seen in Fig. 6 to grow, up to about µY1 = -0.3. This is an important fact:
in the oscillatory regime, with large control flows, the effective return (suction) flow in
the exit nozzles are substantially higher than what might be expected by considering the
zero control f..................[:=> 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 y..................[:=> 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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se..................[:=> 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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xture engines, nitrogen oxide emission must be reduced. This can be done by catalyst or exhaust recirculation in the engine. However research continues to make lean burn engines ecologically viable...................[:=> 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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y calculates and precisely controls the fuel flow rate to the engines giving precise thrust. In addition to the fuel metering function, the FADEC performs numerous other control and monitoring functions such as Variable Stator Vanes (VSV's) and Variable Bleed Valves (VBV's) control, cabin bleeds and power off-takes control, control of starting and re-starting, turbine blade and vane cooling and blade tip clearance control, thrust reversers control, engine health monitoring, oil debris monitoring and vibration monitoring. The inputs come from various aircraft and engine sensors. Apart from the ..................[:=> Show Contents <=:]



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