Consider a Pitot static tube mounted on the nose of an experimental airplane. APitot tube measures the total pressure at the tip of the probe (hence sometimes calledthe Pitot pressure), and a Pitot static tube combines this with a simultaneousmeasurement of the free-stream static pressure. The Pitot and free-stream staticmeasurements are given below for three different flight conditions. Calculate the free-stream Mach number at which the airplane is flying for each of the three differentconditions:(a) Pitot pressure = 1.22 x 10° N/m', static pressure = 1.01 x 10° N/m(b) Pitot pressure = 3.413 atm, static pressure = 1 atm.(c) Pitot pressure = 6.194 atm, static pressure = 0.482 atm.

(a) Given that Pitot pressure is : Po=1.22×105 N/m2 Static pressure is :P=1.01×105 N/m2 Now we…

Consider a Pitot static tube mounted on the nose of an experimental airplane. A itot tube measures the total pressure at the tip of the probe (hence sometimes called e Pitot pressure), and a Pitot static tube combines this with a simultaneous easurement of the free-stream static pressure. The Pitot and free-stream static easurements are given below for three different flight conditions. Calculate the free- ream Mach number at which the airplane is flying for each of the three different onditions: (a) Pitot pressure = 1.22 x 10° N/m´, static pressure = 1.01 x 10 N/m² (b) Pitot pressure = 3.413 atm, static pressure = 1 atm. (c) Pitot pressure = 6.194 atm, static pressure = 0.482 atm. %3D %3D

Consider a Pitot static tube mounted on the nose of an experimental airplane. A itot tube measures the total pressure at the tip of the probe (hence sometimes called e Pitot pressure), and a Pitot static tube combines this with a simultaneous easurement of the free-stream static pressure. The Pitot and free-stream static easurements are given below for three different flight conditions. Calculate the free- ream Mach number at which the airplane is flying for each of the three different onditions: (a) Pitot pressure = 1.22 x 10° N/m´, static pressure = 1.01 x 10 N/m² (b) Pitot pressure = 3.413 atm, static pressure = 1 atm. (c) Pitot pressure = 6.194 atm, static pressure = 0.482 atm. %3D %3D

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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