توجه: محتویات این صفحه به صورت خودکار پردازش شده و مقاله‌های نویسندگانی با تشابه اسمی، همگی در بخش یکسان نمایش داده می‌شوند.
۱Component Integration in CBS Development: A Review
نویسنده(ها): ، ، ،
اطلاعات انتشار: همایش ملی مهندسی رایانه و مدیریت فناوری اطلاعات، سال
تعداد صفحات: ۵
Component integration is identified as a procedure that performs a fundamental role in overallComponent Based System Development (CBSD). According to the integration–based character of CBSdevelopment, a system integrator focuses on assembling of existing components which are developed bydifferent parts to create a software system. For this reason, CBS integration is a risk–prone process becauseit occurs rarely that all the components are totally matched together and ready for ‘plug and play’.Furthermore, one of the most important concerns in CBS development is the absence of componentdocumentation detailed owing to its significant influence on the integration phase of a CBS development lifecycle.In this research, the most important points about component documentation and risk factors duringcomponent integration process have been reviewed.<\div>

۲Nanofluids Convection Heat Transfer inside Closed Conduits: A Review
نویسنده(ها): ، ، ،
اطلاعات انتشار: دومین همایش ملی فناوری نانو از تئوری تا کاربرد، سال
تعداد صفحات: ۹
Application of nano fluids in heat transfer enhancements is prospective. They are well suited to heat transfer. A number of studies on effect of nanofluids in heat transfer have been conducted in order to determine the enhancement properties in addition to control factors configurations. The principal objective of the present study is to elaborate on current research based on the natural, forced and the mixed convective heat transfer characteristics of nanofluids for single– and two– phase models exclusively. Convection of nanofluids in various closed conduits is reviewed both numerically and experimentally.<\div>

۳Turboprop Engine efficiency at On–design Condition
نویسنده(ها): ، ، ،
اطلاعات انتشار: دومین کنفرانس بین المللی دستاوردهای نوین در علوم مهندسی و پایه، سال
تعداد صفحات: ۸
Efficiency of a turboprop engine equipped by Clark–Y 5868–R9 propeller is studied numerically at ondesignconditions. To obtain the efficiency of the propeller, the thrust and power coefficients and alsoperformance of the propeller are calculated. At on–design condition, the object of cycle analysis is to obtainestimates of the performance in terms of design limitations such as flight conditions, and design choices. Theprovided house–made code predict some performance parameters such as overall thermal efficiency, compressorpressure ratio, fuel flow rate, specific fuel consumption and turbine inlet temperature versus various altitudes andflight Mach numbers. It can be seen that in a specified altitude and also due to increasing flight Mach number thecompressor pressure ratio will be abate and the specific thrust will be decreased. As a result of increasing flightMach number and in a given elevation, the specific fuel consumption (SFC) will be increase. Also, reducing thetemperature of air at entry to a turboprop engine will increase the specific thrust. So, liquid injection methodused to increase temperature of the air which entry to the turboprop engine.<\div>
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