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SonTek/YSI Argonaut-XR Technical Manual - HydroScientific West

SonTek/YSI Argonaut-XR Technical Manual - HydroScientific West

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<strong>Argonaut</strong> Principles of Operation (March 1, 2001)<br />

<strong>SonTek</strong>/<strong>YSI</strong><br />

The wave spectral estimates are presented as an array of coefficients, each giving the mean wave<br />

amplitude (square root of the energy) within a period band. Ten bands are used, which<br />

correspond to two-second periods ranging over 2-20+ seconds.<br />

For each band, the <strong>Argonaut</strong> computes and reports the mean wave amplitude (A) for waves<br />

within the period range in the band. If Ai is the amplitude for band, i, the total wave energy is<br />

given by:<br />

Total energy (σA 2 ) = Σ( Ai 2 ) for i=1 to 10<br />

A generally accepted estimate of the significant wave height can be easily obtained from the<br />

amplitudes using:<br />

Hmo=4 * √(Total energy)<br />

6.5. Sound Speed<br />

The <strong>Argonaut</strong> uses sound speed to convert the Doppler shift to water velocity. This section<br />

discusses how to correct <strong>Argonaut</strong> velocity data for errors in the sound speed used for data<br />

collection. Since the <strong>Argonaut</strong> uses an internal temperature sensor for automatic sound speed<br />

compensation, user corrections are rarely needed.<br />

In shallow water, the speed of sound in water is a function of temperature and salinity. Generally,<br />

a temperature change of 5°C or a salinity change of 12 ppt results in a change in sound speed of<br />

one percent. The full range of typical temperature and salinity levels, from -5 to 50°C and 0 to<br />

60 ppt, gives a sound speed range of 1375 to 1600 m/s (total change of 14%). <strong>SonTek</strong> can<br />

provide an algorithm for sound speed calculations upon request.<br />

<strong>Argonaut</strong> velocities scale directly with sound speed: a 1% error in sound speed results in a 1%<br />

error in velocity measurements. The following formula is used for postprocessing corrections and<br />

can be directly applied to the output velocity data of the <strong>Argonaut</strong>.<br />

Where<br />

Vtrue = Vorig (Ctrue / Corig)<br />

Vtrue = Corrected velocity measurements<br />

Vorig = Uncorrected (original) velocity measurements<br />

Ctrue = True speed of sound<br />

Corig = Speed of sound used in original calculations<br />

Errors in sound speed also affect the physical location of the <strong>Argonaut</strong> measurement volume,<br />

although these errors are generally very small. To calculate the correct location of the <strong>Argonaut</strong><br />

measurement volume, use the formula:<br />

Where<br />

Ztrue = Zorig (Ctrue / Corig)<br />

Ztrue = Corrected measurement volume location<br />

Zorig = Uncorrected (original) measurement volume location<br />

Ctrue = True speed of sound<br />

Corig = Speed of sound used in original calculations<br />

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