engine.pipeline.stability.acoustic.GasState Class Reference

Static Public Attributes
float	mach_nozzle_entrance = 0.2
Optional	prandtl = None

Detailed Description

Chamber gas + nozzle conditions needed for the damping budget.

Definition at line 54 of file acoustic.py.

Member Data Documentation

mach_nozzle_entrance

float engine.pipeline.stability.acoustic.GasState.mach_nozzle_entrance = 0.2

static

Definition at line 59 of file acoustic.py.

prandtl

Optional engine.pipeline.stability.acoustic.GasState.prandtl = None

static

Definition at line 60 of file acoustic.py.

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

• EngineDesign/engine/pipeline/stability/acoustic.py