Example $11\mathrm{.}2$ Stagnation Properties

An airliner cruises at $250\frac{m}{s}$ at an altitude of $10$ km above sea level.

a$)$ Calculate the stagnation pressure and temperature relative to the airliner.

b$)$ Compute the same quantities for a speed of $500\frac{m}{s}$ at the same altitude.

Example $11\mathrm{.}2$ Stagnation Properties

An airliner cruises at $250\frac{m}{s}$ at an altitude of $10$ km above sea level.