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   journal of thermal science and technology   
سال:2015 - دوره:35 - شماره:2


  tick  Artificial Neural Network based prediction of time-dependent behavior for lid-driven cavity flows - صفحه:1-18

  tick  Development of a thermal mathematical model for the simulation of transient behavior of a spaceborne equipment in vacuum environment - صفحه:37-44

  tick  Development of semi-spherical porous metal matrix burner for combies - صفحه:137-143

  tick  Devised application of LabView for an automatic test system based on generation,control and processing of pulsatile pipe flows - صفحه:75-88

  tick  Drying kinetics of sewage sludge and hazelnut shell mixtures used as an alternative fuel in cement industry - صفحه:45-52

  tick  Effect of hydrogen enriched diesel combustion on emissions and engine performance at partial load conditions - صفحه:107-117

  tick  Effect of spoilers to pressure distribution on building roof surfaces - صفحه:119-127

  tick  Effect of the air flow rate of blower on the performance of solar still - صفحه:145-152

  tick  Experimental investigations of thermal conductivity,thermal degradation and fire resistance of rigid polyurethane foams filled with nanocalcite and intumescent flame retardant - صفحه:63-74

  tick  Investigation on the relation between exergy loss and NTU - صفحه:153-164

  tick  Nonlinear heat transfer in rectangular fins and exact solutions with temperature dependent properties - صفحه:29-35

  tick  Numerical analysis of combined natural convection and radiation in a square enclosure partially heated vertical wall - صفحه:99-106

  tick  Optimum spacing between horizontal metal hydride (MH) hydrogen storage tanks integrated with fuel cell power system in natural convection - صفحه:129-135

  tick  Performance,emission and combustion characteristics of bioethanol-biodiesel-diesel fuel blends used in a common rail diesel engine - صفحه:19-27

  tick  Second law analysis of different refrigerants in a two stage vapor compression cycle - صفحه:89-97

  tick  Sizing of a turboprop unmanned air vehicle and its propulsion system - صفحه:53-62
 

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