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$1$

Problem $04\mathrm{.}060-$ Calculate Mach number and pressure sensed by Pitot tube

$11\mathrm{.}11$

points

The maximum velocity of the Lockheed F$-104$ is $1328$ mph at an altitude of $37000$ ft $.$ Calculate the Mach number of the airplane and the pressure sensed by a Pitot tube on the airplane. Refer to the Appendix shown below for standard values.

$\backslash$table$[[$Altitude$,,,],[$h$\_($G$,),$ft$,$h$,$ft$,,,],[33,500,33,446,,,],[34,000,33,945,399\mathrm{.}41,5\mathrm{.}3589+2,7\mathrm{.}8165-4],[34,500,34,443,397\mathrm{.}64,5\mathrm{.}2347,7\mathrm{.}6696],[35,000,34,941,395\mathrm{.}86,5\mathrm{.}1129,7\mathrm{.}5247],[35,500,35,440,394\mathrm{.}08,4\mathrm{.}9934,7\mathrm{.}3820],[36,000,35,938,392\mathrm{.}30,4\mathrm{.}8762,7\mathrm{.}2413],[36,500,36,436,390\mathrm{.}53,4\mathrm{.}7612,7\mathrm{.}1028],[37,000,36,934,389\mathrm{.}99,4\mathrm{.}6486,6\mathrm{.}9443],[37,500,37,433,389\mathrm{.}99,4\mathrm{.}5386,6\mathrm{.}7800],[38,000,37,931,389\mathrm{.}99,4\mathrm{.}4312,6\mathrm{.}6196],[,,389\mathrm{.}99,4\mathrm{.}3263,6\mathrm{.}4629]]$

The Mach number of the airplane is

The pressure sensed by the pitot tube is $3618l\frac{b}{f}{t}^2.$