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Displacement and momentum thickness around Naca 0012 in a Transonic Flow

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June 22, 2013, 11:32	Displacement and momentum thickness around Naca 0012 in a Transonic Flow	#1
moh.sob New Member Mohammad Sobhani Join Date: Sep 2012 Location: Iran, Tehran Posts: 8 Rep Power: 13	Hi everybody ! I'm simulating flow around a Naca 0012 airfoil with angle of attack 1.25 (degree) and farfield mach number 0.8. The results for displacement thickness and momentum thickness are shown in 2 graphs in following links. http://inspic.com/4412C0D6 http://inspic.com/42B9FFCD In all field, both of thickness are negative. Are they correct ?

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displacement thickness, fluent, momentum thickness, naca 0012, transonid

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