Help with NSC2KE program
I've downloaded the NSC2KE software from the net and I'm using it with good results studying an hypersonic turbulent compression corner. I need help though to derive from the program's output the wall Stanton Number or the wall heat flux. In one of the tutorial examples of the program there's a similar case with graphs for St but I didn't find how the autor calculated them.
Thanks in advance
PS: sorry for my english and this "poor" question
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