public final class StdAtmos1962 extends StdAtmos
Modified by: Joseph A. Huwaldt
Constructor and Description |
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StdAtmos1962()
Constructor that assumes an altitude of 0 meters,
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StdAtmos1962(double altitude)
Constructor taking a value of geometric 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 1962 standard atmosphere.
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double |
maxAltitude()
Returns the maximum altitude supported by this
atmosphere model.
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double |
minAltitude()
Returns the minimum altitude supported by this
atmosphere model.
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double |
P0()
Returns the standard sea level pressure for this
atmosphere model.
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double |
RHO0()
Returns the standard sea level density for this
atmosphere model.
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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.
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getAltitude, getDensity, getDensityRatio, getPressure, getPressureRatio, getSpeedOfSound, getSpeedOfSoundRatio, getTemperature, getTemperatureRatio, toString
public StdAtmos1962()
public StdAtmos1962(double altitude) throws java.lang.IllegalArgumentException
altitude
- The geometric altitude above MSL at which the 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
- The geometric altitude above MSL at which standard atmosphere is to
be calculated (in meters).java.lang.IllegalArgumentException
public static void main(java.lang.String[] args)