A model airplane has dimensions that are 1/16 those of its prototype. It is desired to test it in a pressure wind tunnel
Posted: Fri Jul 08, 2022 5:49 am
A model airplane has dimensions that are 1/16 those of its prototype. It is desired to test it in a pressure wind tunnel at a speed the same as that of the prototype. If the air temperature is the same and the Reynolds number is the same, what must be the I pressure in the wind tunnel relative to the atmospheric pressure?