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Gaseous flow over an airfoil is always compressible because of very high compressibility value of gases.(a) Always true(b) Always false(c) True only for high speeds(d) True for low speedsI have been asked this question during an interview.I'd like to ask this question from Definition of Compressibility in division Compressible Flow – Preliminary Aspects of Aerodynamics |
Answer» The CORRECT answer is (C) True only for high speeds |
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