The pressure rise from free stream to the nose of the fuselage section of an aircraft is
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The pressure rise from free stream to the nose of the fuselage section of an aircraft is measured in a wind tunnel at 20 degrees Celsius to be 34 KPa with a wind tunnel air a speed of 900 km/hr. If the test is to simulate flight at an elevation of 12km, what is the prototype velocity and the expected nose pressure rise?
Related Book For
Thermodynamics An Engineering Approach
ISBN: 978-0073398174
8th edition
Authors: Yunus A. Cengel, Michael A. Boles
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