Finally someone puts the nail in it ... find the heat on the turbine see it will melt them readjust for a temp and compression that wont melt them .... now we see where the brain sweat hits the paper ... and gets put to use in an actual need and compromise
As an gas turbine engineer, i appreciate your work, that is some quality content right here👌
Finally someone puts the nail in it ... find the heat on the turbine see it will melt them readjust for a temp and compression that wont melt them .... now we see where the brain sweat hits the paper ... and gets put to use in an actual need and compromise
Amazing video thank you
Hey Roddy, I am doing a similar assignment regarding two spool jet engine, but I am difficulty doing it, are you able to help out?
Is it simply Compressor ratio or compressor pressure ratio is different from that!!!
Compressor Pressure Ratio is more correct, but I may have used both terms to represent the same thing.
@@RoddyMcNamee thanks alot sir.,....,from India❤️
@@Iris0555 thank you for watching and for the positive comments. It helps to motivate me to do more.
Therefore at 20X compression you will be just fine
the calculation is wrong, the sp. heat cap. for air is 1,005 not 1.005 J/g-1K-1
nope he used KiloJoules not Joules ... 1005j is 1.005Kj .... you just havent used metric long enough to figure out 1,000 = 1 kilo