Hi,
Im an aeronautical engineer. Im spent much of my career working on gas turbine (jet) engines.
Ive worked as a specialist engineer in Rolls Royce, now in Gasturbine Research Establishment.
This project is more like my regular work. I just have one question. The numerical values required for the calculation - are those supposed to be taken from the attached graphs in the document. Please clarify on this.
Apart from this , as you want, i can guarantee 100% project. nothing less. maybe more .
please feel free to contact me anytime
Regards
Aeromaster