To find the drag on an airplane whose velocity is 167 ms

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Reference no: EM13630777

To find the drag on an airplane whose velocity is 167 m/s, could one test a 1 : 25 scale model in a subsonic (local match number less than one) wind tunnel at the same pressure and temperature if the reynolds number is the only II-group the drag depends on?

Reference no: EM13630777

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