Engineering, 21.12.2019 06:31 gugu1004
An airplane, of overall length 55 ft, is designed to fly at 680 m/s at 8000-m standard altitude. a one-thirtieth-scale model is to be tested in a pressurized helium wind tunnel at 20°c. what is the appropriate tunnel pressure in atm? even at this (high) pressure, exact dynamic similarity is not achieved. why?
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An airplane, of overall length 55 ft, is designed to fly at 680 m/s at 8000-m standard altitude. a o...
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