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 1 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.](https://theskyscorner.com/wp-content/uploads/2023/03/image-187.png)
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.