An on-line course I had recently created is about Advanced Power Conversion Analysis, and it presents the best, very simple and standard power cycles (Carnot Cycle, Brayton Cycle, Otto Cycle and Diesel Cycle), excellent power cycle elements/processes (compression, combustion and expansion) and excellent compressible flow elements (subsonic nozzle, diffuser and thrust).

When dealing with energy cycles two different approaches are taken with respect to the functioning fluid. For Carnot Cycle and Brayton Cycle, air argon, helium and nitrogen are deemed as the functioning fluid. For Otto Cycle and Diesel Cycle, only air is utilised as the operating fluid.

When dealing with power cycle components/processes (compression and expansion) and compressible flow (nozzle, diffuser and thrust), air, argon, helium and nitrogen are utilised as the operating fluid.

When dealing with combustion, six unique fuels (carbon, hydrogen, sulfur, coal, oil and gas) react with air and oxygen enriched air as the oxidant at unique stoichiometry values (stoichiometry => 1) and oxidant input temperature values.

For each and every energy cycle thermal efficiency derivation is presented with a basic mathematical method. Also, for every single energy cycle, a T – s diagram and energy cycle major functionality trends (thermal efficiency, specific power output, power output, combustion products on weight and mole basis, distinct fuel consumption and stoichiometry) are plotted in a20few figures as a function of compression stress ratio, turbine inlet temperature and/or final combustion temperature and operating fluid mass flow rate. It ought to be noted that this on-line course does not deal with costs (capital, operational or upkeep).

For compression and expansion, the technical performance of mentioned energy cycle components/processes is presented with a given connection involving pressure and temperature. While for combustion, the technical efficiency at stoichiometry => 1 circumstances and is presented being aware of the enthalpy values for combustion reactants and goods, given as a function of temperature.

This course delivers the compression and expansion T – s diagrams and their key performance trends plotted in a few figures as a function of compression and expansion stress ratio and functioning fluid mass flow rate. For combustion circumstances regarded as, fuel higher heating value (HHV) or enthalpy of combustion, flame temperature and oxidant to fuel ratio are presented in tabular form and plotted in a few figures. Also, both weight and mole basis combustion solutions are offered in tabular kind and plotted in a handful of=2 0figures.

For dailydriven.ro/cati-cai-putere-are-un-kw , diffuser and thrust, the technical overall performance of pointed out compressible flow elements is presented with a offered relationship involving pressure and temperature as a function of Mach Number. This course supplies the compressible flow components T – s diagrams and their key functionality trends (stagnation over static temperature and pressure) are plotted in a handful of figures as a function of the Mach Number.

Boost your expertise on advanced combustion evaluation and Advanced Energy Conversion Evaluation, by taking my course on the Coggno Marketplace for online coaching and elearning.