A Pitot tube is used to find stagnation pressure in relation to the static pressure port in an aircraft. The aircraft is flying at an altitude of 10 kilometers on a standard day. The pressure that is measured is 16.4 kPa gage. Find the following: 1.) Atmospheric conditions at an altitude of 10 kilometers, use online resources if needed 2.) If you assume the flow is incompressible, find the following: a. The flight speed b. Mach number of the aircraft

A Pitot tube is used to find stagnation pressure in relation to the static pressure port in an aircraft. The aircraft is flying at an altitude of 10 kilometers on a standard day. The pressure that is measured is 16.4 kPa gage. Find the following: 1.) Atmospheric conditions at an altitude of 10 kilometers, use online resources if needed 2.) If you assume the flow is incompressible, find the following: a. The flight speed b. Mach number of the aircraft

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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