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Physics, 09.10.2019 23:00 MariaIZweird9631

A40% scale model of an airplane is to be tested in a flow regime where unsteady flow effects are important. if the full-scale vehicle experiences the unsteady effects at a mach number of 1 at an altitude of 40,000 ft, what pressure must the model be tested at to produce an equal reynolds number? the model is to be tested in air at 70 f. what will the timescale of the flow about the model be relative to the full-scale vehicle?

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