Gauging Thrust Figures

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KJ_Lesnick

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I'm wondering if there's any mathematical formulae for either determining precise static non-afterburning thrust levels, or at least good guesstimate figures based on the following parameters
  • Engine inlet-diameter
  • Mass-flow
  • Pressure-ratio
  • Ratio of inlet to nozzle diameter
  • Other
Since I'm not a propulsion engineer, nor am an the best at math, I do effectively need to know what units to enter in (i.e. metric and things of that sort).




BTW: Everybody tells me to do my own research and this will help me do exactly that without having to pester everybody
 

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