feedtwin.engine.chamber.CombustionState Class Reference

Static Public Attributes
float	temperature = 0.0
float	gamma = 0.0
float	thrust_coefficient = 0.0
bool	extrapolated = False

Detailed Description

What the gas in the chamber is doing.

Definition at line 45 of file chamber.py.

Member Data Documentation

extrapolated

bool feedtwin.engine.chamber.CombustionState.extrapolated = False

static

Definition at line 60 of file chamber.py.

gamma

float feedtwin.engine.chamber.CombustionState.gamma = 0.0

static

Definition at line 54 of file chamber.py.

Referenced by test_combustion_stability_audit.TestNyquistAllCrossings.case(), feedtwin.engine.chamber.ConstantCStar.combustion(), test_combustion_stability_audit.TestNyquistAllCrossings.L_indep(), and engine.pipeline.stability.chug.ChugChamber.theta_c().

temperature

float feedtwin.engine.chamber.CombustionState.temperature = 0.0

static

Definition at line 51 of file chamber.py.

Referenced by feedtwin.session.network_trace.NetworkTrace.append(), feedtwin.engine.design.InjectorSide.cd_at(), feedtwin.engine.chamber.ConstantCStar.combustion(), feedtwin.vessels.volume.GasVolume.rates(), feedtwin.session.network_trace.NetworkTrace.record(), and feedtwin.session.burn.BurnTrace.recorder().

thrust_coefficient

float feedtwin.engine.chamber.CombustionState.thrust_coefficient = 0.0

static

Definition at line 57 of file chamber.py.

Referenced by feedtwin.engine.chamber.ConstantCStar.combustion().

---

The documentation for this class was generated from the following file:

• lib/feedtwin/feedtwin/engine/chamber.py