Class ThrusterMathLibrary

Namespace

NominalSystems.Classes

Assembly

NominalSystems.Classes.dll

[NominalSystems] A collection of mathematical functions

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public static class ThrusterMathLibrary

Inheritance

object

ThrusterMathLibrary

Methods

CompressibleAreaRatio(double, double)

Area ratio function for a compressible flow in the supersonic regime

public static double CompressibleAreaRatio(double gamma, double M = 1)

Parameters

gamma double

Specific heat ratio

M double

Mach Exit

Returns

double

The Area Ratio

NewtonRaphson(Func<double, double>, double)

Generalized Newton Raphson method

public static double NewtonRaphson(Func<double, double> func, double delta = 1E-06)

Parameters

func Func<double, double>

Function passed in for root finding

delta double

Accuracy of root finding method

Returns

double

Returns the root of the function

ThrusterMachExit(double, double)

Calculates the Exit Mach Number using the Area Ratio of throat and exit of the nozzle using Newton Raphson's method of root finding

public static double ThrusterMachExit(double gamma, double a_star)

Parameters

gamma double

a_star double

Returns

double