Physics for Scientists and Engineers
6th Edition
ISBN: 9781429281843
Author: Tipler
Publisher: MAC HIGHER
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The aircraft fuselage can be approximated as a circular cylinder for non-viscous aerodynamicanalysis. Given that the surface velocity of inviscid flow around a circular cylinder is:V = 2U∞sinθWhere q = 0 is a point on the axis of symmetry, show that the maximum dynamic pressure on thecylinder amounts to: 2 ρU∞2If P∞ at some distance upstream of the cylinder is 100kPa, and U∞ is 50m/s, determine the minimumstatic pressure on the cylinder surface for an air flow with density 1.225kg/m3
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Chapter 13 Solutions
Physics for Scientists and Engineers
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