EBK MUNSON, YOUNG AND OKIISHI'S FUNDAME
8th Edition
ISBN: 9781119547990
Author: HOCHSTEIN
Publisher: JOHN WILEY+SONS INC.
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Chapter 11.1, Problem 2P
(a)
To determine
The change in specific internal energy between the section 1 and 2.
(b)
To determine
The change in specific enthalpy between the section 1 and 2.
(c)
To determine
The change in density between the section 1 and 2.
(d)
To determine
The change in specific entropy between the section 1 and 2.
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An AISI 1018 steel ball with 1.100-in diameter is used as a roller between a flat plate
made from 2024 T3 aluminum and a flat table surface made from ASTM No. 30 gray
cast iron. Determine the maximum amount of weight that can be stacked on the
aluminum plate without exceeding a maximum shear stress of 19.00 kpsi in any of the
three pieces. Assume the figure given below, which is based on a typical Poisson's
ratio of 0.3, is applicable to estimate the depth at which the maximum shear stress
occurs for these materials.
1.0
0.8
Ratio of stress to Pmax
0.4
90
0.6
στ
Tmax
0.2
0.5a
a
1.5a
2a
2.5a
За
Distance from contact surface
The maximum amount of weight that can be stacked on the aluminum plate is
lbf.
A carbon steel ball with 27.00-mm diameter is pressed together with an aluminum ball
with a 36.00-mm diameter by a force of 11.00 N. Determine the maximum shear
stress and the depth at which it will occur for the aluminum ball. Assume the figure
given below, which is based on a typical Poisson's ratio of 0.3, is applicable to estimate
the depth at which the maximum shear stress occurs for these materials.
1.0
0.8
Ratio of stress to Pma
9 0.6
στ
24
0.4
Tmax
0.2
0
0.5a
a
1.5a
Z
2a
2.5a
За
Distance from contact surface
The maximum shear stress is determined to be
MPa.
The depth in the aluminum ball at which the maximum shear stress will occur is
determined to be [
mm.
Chapter 11 Solutions
EBK MUNSON, YOUNG AND OKIISHI'S FUNDAME
Ch. 11.1 - Prob. 1PCh. 11.1 - Air flows steadily between two sections in a duct....Ch. 11.1 - Consider the flow process in Fig. P11.3. Does the...Ch. 11.1 - Prob. 4PCh. 11.1 - Prob. 5PCh. 11.1 - Prob. 6PCh. 11.1 - Prob. 7PCh. 11.1 - Prob. 8PCh. 11.1 - Air flows in a 15-cm-diameter horizontal pipe. At...Ch. 11.1 - An air heater in a large coal-fired steam...
Ch. 11.2 - Determine the static pressure to stagnation...Ch. 11.2 - Prob. 12PCh. 11.2 - Prob. 13PCh. 11.2 - Prob. 14PCh. 11.2 - Prob. 15PCh. 11.3 - Prob. 16PCh. 11.3 - Prob. 17PCh. 11.3 - Prob. 18PCh. 11.3 - Prob. 19PCh. 11.3 - Prob. 20PCh. 11.3 - Prob. 21PCh. 11.3 - Prob. 22PCh. 11.4 - Prob. 23PCh. 11.4 - Prob. 24PCh. 11.4 - Prob. 25PCh. 11.4 - Prob. 26PCh. 11.4 - Prob. 27PCh. 11.4 - Air flows in a constant-area, insulated duct. The...Ch. 11.5 - Prob. 29PCh. 11.5 - The Pitot tube on a supersonic aircraft (see Video...Ch. 11.5 - An aircraft cruises at a Mach number of 2.0 at an...Ch. 11.5 - Prob. 32PCh. 11.5 - Prob. 33PCh. 11.5 - Prob. 34PCh. 11.5 - Prob. 35PCh. 11.6 - The stagnation pressure and temperature of air...Ch. 11.6 - Prob. 37PCh. 11.6 - Prob. 38PCh. 11.6 - Prob. 39PCh. 11.6 - Prob. 40PCh. 11.6 - Prob. 41PCh. 11.6 - The static pressure to stagnation pressure ratio...Ch. 11.7 - Air flows steadily and isentropically from...Ch. 11.7 - Prob. 44PCh. 11.7 - Prob. 45PCh. 11.7 - Prob. 46PCh. 11.7 - At a certain point in a pipe, air flows steadily...Ch. 11.7 - Prob. 48PCh. 11.7 - Prob. 49PCh. 11.7 - Prob. 50PCh. 11.7 - A jet engine is to be designed for an altitude of...Ch. 11.7 - Prob. 52PCh. 11.7 -
A convergent–divergent nozzle has an exit throat...Ch. 11.7 - An ideal gas flows isentropically through a...Ch. 11.8 - Standard atmospheric air (T0 = 59 F, p0 = 14.7...Ch. 11.8 - Prob. 57PCh. 11.8 - Prob. 58PCh. 11.8 - Prob. 59PCh. 11.8 - Prob. 64PCh. 11.9 - Prob. 66PCh. 11.9 - Prob. 67PCh. 11.9 - Prob. 68PCh. 11.9 - Air enters a frictionless, constant area duct with...Ch. 11.9 - Prob. 70PCh. 11.9 - Prob. 71PCh. 11.9 - Prob. 72PCh. 11.9 - Prob. 73P
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