Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000 View on Open Library

Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000

by Robert D. Van Dyken

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First published: 1997 1 language
Subjects
VORTEX SHEDDING STALLING FLOW SEPARATION BUBBLES

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