Fundamentals of Aerodynamics
Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259129919
Author: John D. Anderson Jr.
Publisher: McGraw-Hill Education
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Chapter 10, Problem 10.10P

A 20 ° half-angle wedge is mounted at 0 ° angle of attack in the test section of a supersonic wind tunnel. When the tunnel is operating, the wave angle from the wedge leading edge is measured to be 41 . 8 ° . What is the exit-to-throat area ratio of the tunnel nozzle?

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25 mm 10 mm 250 mm a 15 mm 250 mm 0.3 m (300 mm) A n 65 kN 90 kN 65 kN B PROBLEM 6.11 For the beam and loading shown, consider section n-n and determine (a) the largest shearing stress in that section, (b) the shearing stress at point a. 15 mm 0.6 m 0.6 m 0.6 m 0.6 m
A 000 RA 1.8 m P W610 X 155 C B 2.7 m- RC PROBLEM 6.17 For the wide-flange beam with the loading shown, determine the largest load P that can be applied, knowing that the maximum normal stress is 165 MPa and the largest shearing stress using the approximation T = VIA web is 100 MPa.
PROBLEM 6.31 The built-up beam shown is made up by gluing together five planks. Knowing that the allowable average shearing stress in the glued joints is 400 kPa, determine the largest permissible vertical shear in the beam. 50 mm 100 mm 50 mm 125 50 125 mm mm mm
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