Asked for analysis on Water Swirled into Hot End gas turbine Combined Cycle with extractive turbine after or thrust gas aircraft propulsion enhancement increase!
Thermodynamic analysis preliminary with many assumptions Net Thrust Gas Volume Increase about = 23 % Factors in the analysis being worked on
1. Size of Water Droplets Created by Nozzle Parameters &/or Impingement Design Detail. &/or rotational design / Start point - “Perry's Chemical Engineers' Handbook, Eighth Edition” 12.2. EVAPORATIVE COOLING
- Spacing of droplets 12.2. EVAPORATIVE COOLING
- Inter-activeness of vaporization visa vi temperature gas - liquid visa vi cooling of mass visa vi turbulence 5.4. HEAT TRANSFER WITH CHANGE OF PHASE and “Handbook of Energy Engineering Calculations” by: Tyler G. Hicks, P.E., .
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