public final class StdAtmos1976 extends StdAtmos
Modified by: Joseph A. Huwaldt
Constructor and Description |
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StdAtmos1976()
Constructor that assumes an altitude of 0 meters,
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StdAtmos1976(double altitude)
Constructor that takes a value of altitude in meters.
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Modifier and Type | Method and Description |
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double |
a0()
Returns the standard sea level speed of sound for this
atmosphere model.
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static void |
main(java.lang.String[] args)
A simple method to test the 1976 standard atmosphere.
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double |
maxAltitude()
Returns the maximum altitude supported by this
atmosphere model in meters.
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double |
minAltitude()
Returns the minimum altitude supported by this
atmosphere model in meters.
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double |
P0()
Returns the standard sea level pressure for this
atmosphere model in Newtons/m^2.
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double |
RHO0()
Returns the standard sea level density for this
atmosphere model in kg/L (g/cm^3).
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void |
setAltitude(double altitude)
Sets the geometric altitude where the standard atmosphere
is to be calculated.
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double |
T0()
Returns the standard sea level temperature for this
atmosphere model in Kelvin.
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getAltitude, getDensity, getDensityRatio, getPressure, getPressureRatio, getSpeedOfSound, getSpeedOfSoundRatio, getTemperature, getTemperatureRatio, toString
public StdAtmos1976()
public StdAtmos1976(double altitude) throws java.lang.IllegalArgumentException
altitude
- Altitude at which standard atmosphere is to be
calculated; value given in meters.java.lang.IllegalArgumentException
public final double T0()
public final double P0()
public final double RHO0()
public final double a0()
public double minAltitude()
minAltitude
in class StdAtmos
public double maxAltitude()
maxAltitude
in class StdAtmos
public void setAltitude(double altitude) throws java.lang.IllegalArgumentException
setAltitude
in class StdAtmos
altitude
- Geometric altitude at which standard atmosphere is to be
calculated; value given in meters.java.lang.IllegalArgumentException
public static void main(java.lang.String[] args)