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Some Air Standard Cycles (Theoretical Brayton Cycles)

Vers 1.7(this)/1.2(airPlot)/1.4(plotClass)/1.4(thermoDraw)        DISCLAIMER

You can animate four air standard cycles. Use the radio buttons to toggle between engine and plot types. If you change parameters such as compression ratio remember to replot the cycle. Use the animate_next_step button to animate each process in the cycle in turn. You can click anywhere on the process plot to list the local values of p, v, T, u, h, s at the point of interest(tabulated below the plot). The add process plot drop down box allows you to plot curves through the POI for comparison against the cycle. Elsevier provide a useful set of articles concerning air standard cycles .

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Engine

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Process Diagram

Replot cycle.

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Choose engine type: Brayton Cycle Brayton Cycle with Regenerator Brayton Cycle with Intercooling and Reheat Turbojet Cycle
Choose plot type: pressure vs volume temperature vs entropy

Engine parameters 1: Mass flow rate: kg/s ; Intake pressure: bar ; Pressure ratio : ; Inlet Temperature: K; (Primary) heat addition rate: kW

Engine parameters 2: isentropic efficiency (compression, %) isentropic efficiency (expansion, %)

Engine parameters 3: ---

Replot cycle. Add process plot through POI Replot cycle. Replot cycle.

Thermodynamic state at POI
pressure, bar temperature, K sp. vol, m^3/kg vol, litres enthalpy, kJ/kg int. en., kJ/kg entropy, kJ/kg K
-- -- -- -- -- -- --
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Energy Flows for each Process
Process Heating rate, kW Shaft power, kW ΔKE, kW ΔH kW
1-2 -- -- -- --
2-3 -- -- -- --
3-4 -- -- -- --
4-5 -- -- -- --
5-6 -- -- -- --
6-7 -- -- -- --
7-8 -- -- -- --
8-1 -- -- -- --
total -- -- -- --

Cycle Efficiency Calculations.

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Heat addition rate: |Q H| = --

Heat rejection rate: |Q L| = --

Cycle power: |W| = --

ηcycle = |W|/|QH| = --

Or, ηcycle = --

Or, ηcycle = --

Thrust Calculations - Applies to Turbojet Only.

Relative velocity at intake, v1 = --

Relative velocity at exhaust, v4 = --

Thrust: F = m (v4-v1) = --

Specific thrust: f = F/m = v4-v1 = --