Example 2. A high-speed AC 130 gunship is flying at a pressure altitude of 10 km. A Pitot tube on the wingtip measures a pressure of 4.24 x 10ª N/m². Calculate the Mach number at which the aircraft is flying. Solution: Solving for P1 at an altitude of 10000 m, we get 2.65 x 104 N/m2 k-1 1.4-1 (P. k 4.24 x 104\ 1.4 %3D - 1 %3D - 1 k – 1 P1 1.4 – 1 2.65 x 104 M2 - 0719

Example 2. A high-speed AC 130 gunship is flying at a pressure altitude of 10 km. A Pitot tube on the wingtip measures a pressure of 4.24 x 10ª N/m². Calculate the Mach number at which the aircraft is flying. Solution: Solving for P1 at an altitude of 10000 m, we get 2.65 x 104 N/m2 k-1 1.4-1 (P. k 4.24 x 104\ 1.4 %3D - 1 %3D - 1 k – 1 P1 1.4 – 1 2.65 x 104 M2 - 0719

Name: Example 2. A high-speed AC 130 gunship is flying at a pressure altitu
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Description: Example 2. A high-speed AC 130 gunship is flying at a pressure altitude of 10 km. APitot tube on the wingtip measures a pressure of 4.24 x 104 N/m². Calculate theMach number at which the aircraft is flying.Solution: Solving for P1 at an altitude of

College Physics

11th Edition

ISBN:9781305952300

Author:Raymond A. Serway, Chris Vuille

Publisher:Raymond A. Serway, Chris Vuille

Chapter1: Units, Trigonometry. And Vectors

Section: Chapter Questions

Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...

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