EBK FUNDAMENTALS OF AERODYNAMICS
6th Edition
ISBN: 9781259681486
Author: Anderson
Publisher: MCGRAW HILL BOOK COMPANY
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Chapter 10, Problem 10.3P
A Pitot tube inserted at the exit of a supersonic nozzle reads
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Problem 4
The semicircular disk has a radius of 0.4 m. At one instant, when 0-60°, it is rotating
counterclockwise at 0-4 rad/s, which is increasing in the same direction at 1 rad/s². Find the
velocity and acceleration of point B at this instant. (Suggestion: Set up relative velocity and
relative acceleration that way you would for a no-slip disk; remember what I told you to memorize
on the first day of class.) (Answer: B = −2.98î - 0.8ĵ m/s, ãB = 2.45î - 5.74ĵ m/s²)
B
0.4 m
y
X
A
C
C
2r
A
2r
B
B
(a)
(b)
Problem 3
Refer to (b) of the figure shown above. The disk OA is now rolling with no slip at a constant angular
velocity of w. Find the angular velocity and angular acceleration of link AB and BC. (Partial Answers:
WBC = 2wk, AB = w²k)
Problem 2
Refer to (a) of the figure shown below, where the disk OA rotates at a constant angular velocity of w.
Find the angular velocity and angular acceleration of link AB and link BC. (Partial Answers: WBC =
wk, AB = w²k)
A 2r
C
B
(a)
A
2r
B
(b)
Chapter 10 Solutions
EBK FUNDAMENTALS OF AERODYNAMICS
Ch. 10 - The reservoir pressure and temperature for a...Ch. 10 - A flow is isentropically expanded to supersonic...Ch. 10 - A Pitot tube inserted at the exit of a supersonic...Ch. 10 - For the nozzle flow given in Problem 10.1, the...Ch. 10 - A closed-form expression for the mass flow through...Ch. 10 - Prob. 10.6PCh. 10 - A convergent-divergent nozzle with an...Ch. 10 - For the flow in Problem 10.7, calculate the mass...Ch. 10 - Consider a convergent-divergent nozzle with an...Ch. 10 - A 20 half-angle wedge is mounted at 0 angle of...
Ch. 10 - The nozzle of a supersonic wind tunnel has an...Ch. 10 - We wish to design a supersonic wind tunnel that...Ch. 10 - Consider a rocket engine burning hydrogen and...Ch. 10 - For supersonic and hypersonic wind tunnels, a...Ch. 10 - Return to Problem 9.18. where the average Mach...Ch. 10 - Return to Problem 9.19, where the average Mach...Ch. 10 - A horizontal flow initially at Mach I flows over a...Ch. 10 - Consider a centered expansion wave where M1=1.0...
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