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Which of these problems does not require three-dimensional analysis?(a) Internal flow in SCRAM jet engines(b) Flow over an aircraft wing(c) Flow past gas turbine compressors(d) Flow over airfoilsI got this question in an international level competition.My question comes from Research and Design Tool topic in section Philosophy of Computational Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct ANSWER is (d) FLOW over airfoils

Best explanation: An airfoil is a two-dimensional profile of a wing. Flow over this two-dimensional profile will not need any three-dimensional ANALYSIS.



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