Source code posted on Github. Apart Github use  info @ basicairdata and socials (see footer) for bug report and feature proposal

Refer to this article for naming conventions and uncertainty. Given the desired maximum Calibrated Airspeed, CAS,  this servlet calculates the maximum differential pressure at the pressure sensor; that info can be used to size the main differential pressure sensor of an ADC. If the coefficient c is set to 1, with no uncertainty, then calculated desired CAS value is equal to Indicated Airspeed, IAS.

The statistical distribution of parameters is assumed to be Gaussian. Confidence level is 99.73%, we considered 3\sigma.

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