3.5. Consider a Pitot static tube mounted on the nose of an experimental airplane Pitot tube measures the total pressure at the tip of the probe (hence sometimes called the Pitot pressure), and a Pitot static tube combines this with a simultaneous measurement of the free-stream static pressure The Pitot and free-stream static measurements 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 different conditions 1 01 x 10$ N/m² (a) Pitot pressure (b) Pitot pressure 1 22 x 10' N/m², static pressure = 1 2116 lb/ft? 1020 lb/ft? 7222 lb/ft?, static pressure %3D (c) Pitot pressure 13107 lb/ft2, static pressure =

3.5. Consider a Pitot static tube mounted on the nose of an experimental airplane Pitot tube measures the total pressure at the tip of the probe (hence sometimes called the Pitot pressure), and a Pitot static tube combines this with a simultaneous measurement of the free-stream static pressure The Pitot and free-stream static measurements 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 different conditions 1 01 x 10$ N/m² (a) Pitot pressure (b) Pitot pressure 1 22 x 10' N/m², static pressure = 1 2116 lb/ft? 1020 lb/ft? 7222 lb/ft?, static pressure %3D (c) Pitot pressure 13107 lb/ft2, static pressure =

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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Question

3.5. Consider a Pitot static tube mounted on the nose of an experimental airplane
Pitot tube measures the total pressure at the tip of the probe (hence sometimes
called the Pitot pressure), and a Pitot static tube combines this with a simultaneous
measurement of the free-stream static pressure The Pitot and free-stream static
measurements 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
different conditions
1 01 x 10$ N/m?
(a) Pitot pressure
(b) Pitot pressure
(c) Pitot pressure
= 1 22 x 10' N/m², static
7222 lb/ft?, static pressure
13107 Ib/ft?, static pressure
pressure
2116 lb/ft?
1020 lb/ft?

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