This study is aimed at investigating the effects of heat loss, as characterized by a percentage of fuel's energy, friction and variable specific heats of the working fluid, on the performance of an air-standard Atkinson cycle under the restriction of the maximum cycle-temperature. A more realistic and precise relationship between the fuel's chemical-energy and the heat leakage is derived through the resulting temperature. The variations in power output and thermal efficiency with compression ratio, and the relations between the power output and the thermal efficiency of the cycle are presented. The results show that the power output as well as the efficiency, for which the maximum power-output occurs, will rise with the increase of maximum ...
Finite-time thermodynamic models for an Otto cycle, an Atkinson cycle, an over-expansion Miller cycl...
This paper presents an analytical study to minimize the heat lost during the power stroke of hydroge...
This paper presents the effect of operation conditions (compression ratio, turbine inlet temperature...
The objective of this study is to examine the influences of heat loss characterized by a percentage ...
Thermodynamic analysis of an ideal air-standard Atkinson cycle with temperature dependant specific h...
Using finite-time thermodynamics, the relations between the power output, thermal efficiency and com...
Performance of an air-standard Atkinson cycle is analyzed by using finite-time thermodynamics. The i...
Thermodynamic analysis of an ideal air standard Atkinson cycle usnder Efficient Power Density is pre...
Effects of heat leakage on the performance characteristics of Carnot like heat engine and heat pump ...
AbstractThe performance of an air standard Miller cycle is analyzed using finite-time thermodynamics...
To simplify analysis of an internal combustion engine, air-standard cycles are conceived. Air is ass...
The influence of the temperature dependence of specific heat capacities of working fluid on specific...
The variability of specific heats, internal irreversibility, heat and frictional losses are neglecte...
Although increasing the turbine inlet temperature has traditionally proved the surest way to increas...
Presented at the 39th AIAA, Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-11, 2001.Thi...
Finite-time thermodynamic models for an Otto cycle, an Atkinson cycle, an over-expansion Miller cycl...
This paper presents an analytical study to minimize the heat lost during the power stroke of hydroge...
This paper presents the effect of operation conditions (compression ratio, turbine inlet temperature...
The objective of this study is to examine the influences of heat loss characterized by a percentage ...
Thermodynamic analysis of an ideal air-standard Atkinson cycle with temperature dependant specific h...
Using finite-time thermodynamics, the relations between the power output, thermal efficiency and com...
Performance of an air-standard Atkinson cycle is analyzed by using finite-time thermodynamics. The i...
Thermodynamic analysis of an ideal air standard Atkinson cycle usnder Efficient Power Density is pre...
Effects of heat leakage on the performance characteristics of Carnot like heat engine and heat pump ...
AbstractThe performance of an air standard Miller cycle is analyzed using finite-time thermodynamics...
To simplify analysis of an internal combustion engine, air-standard cycles are conceived. Air is ass...
The influence of the temperature dependence of specific heat capacities of working fluid on specific...
The variability of specific heats, internal irreversibility, heat and frictional losses are neglecte...
Although increasing the turbine inlet temperature has traditionally proved the surest way to increas...
Presented at the 39th AIAA, Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-11, 2001.Thi...
Finite-time thermodynamic models for an Otto cycle, an Atkinson cycle, an over-expansion Miller cycl...
This paper presents an analytical study to minimize the heat lost during the power stroke of hydroge...
This paper presents the effect of operation conditions (compression ratio, turbine inlet temperature...