Skip to content

A pitot tube mounted on the wing tip measures a pressure of 424 000 Pa

A pitot tube mounted on the wing tip measures a pressure of 424 000 Pa. What will be the Mach number at which the aircraft is flying if the ambient pressure is 265 000 Pa at that altitude? Assume k is 1.3.

A pitot tube mounted on the wing tip measures a pressure of 424 000 Pa. What will be the Mach number at which the aircraft is flying if the ambient pressure is 265 000 Pa at that altitude? Assume k is 1.3.

Leave a Reply

Your email address will not be published. Required fields are marked *