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Calculate the International Standard Atmosphere (ISA) properties at a specified altitude. Temperature offset from ISA conditions is also possible.
Perform hand and true gas turbine performance calculations for turbojets (single and 2-shaft), and mixed and unmixed turbofans (2 and 3-shaft), providing temperatures and pressures between each component. Convergent and Convergent-Divergent nozzles and afterburners are also selectable.
Generate a Weibull or Lognormal distribution for at least two failure points; plot Weibull or Lognormal distributions to visualize one or more distributions; or calculate the convolution of two or more distributions.
Simulate the future fleet risk for a population (and subpopulation) of parts based on changing fleet usage and fleet size. Risk, event rates, removals, procurements, and hazard severity results are generated and plotted.
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