Using numerical results for the Blasius exact solution for laminar boundary-layer flow on a flat plate, (Section 9.2 on the web) plot the dimensionless velocity profile, u / U (on the abscissa), versus dimensionless distance from the surface, y / δ (on the ordinate). Compare with the approximate parabolic velocity profile of Problem 9.8. 9.8 Velocity profiles in laminar boundary layers often are approximated by the equations Linear : u U = y δ Sinusoidal : u U = sin ( π 2 y δ ) Parabolic : u U = 2 ( y δ ) − ( y δ ) 2 Compare the shapes of these velocity profiles by plotting y / δ (on the ordinate) versus u / U (on the abscissa).
Using numerical results for the Blasius exact solution for laminar boundary-layer flow on a flat plate, (Section 9.2 on the web) plot the dimensionless velocity profile, u / U (on the abscissa), versus dimensionless distance from the surface, y / δ (on the ordinate). Compare with the approximate parabolic velocity profile of Problem 9.8. 9.8 Velocity profiles in laminar boundary layers often are approximated by the equations Linear : u U = y δ Sinusoidal : u U = sin ( π 2 y δ ) Parabolic : u U = 2 ( y δ ) − ( y δ ) 2 Compare the shapes of these velocity profiles by plotting y / δ (on the ordinate) versus u / U (on the abscissa).
Using numerical results for the Blasius exact solution for laminar boundary-layer flow on a flat plate, (Section 9.2 on the web) plot the dimensionless velocity profile, u/U (on the abscissa), versus dimensionless distance from the surface, y/δ (on the ordinate). Compare with the approximate parabolic velocity profile of Problem 9.8.
9.8 Velocity profiles in laminar boundary layers often are approximated by the equations
Linear
:
u
U
=
y
δ
Sinusoidal
:
u
U
=
sin
(
π
2
y
δ
)
Parabolic
:
u
U
=
2
(
y
δ
)
−
(
y
δ
)
2
Compare the shapes of these velocity profiles by plotting y/δ (on the ordinate) versus u/U (on the abscissa).
The link lengths and the value of 2 and offset for some fourbar crank-slide linkages are defined
in Table 1. The linkage configuration and terminology are shown in Figure 1. For the rows
assigned, find
(a) all possible solutions for angle & and slider position d by vector loop method.
(b) the transmission angle corresponding to angle 03. (Hint: Treat the vector R4 as virtual rocker)
Show your work in details: vector loop, vector equations, solution procedure.
Table 1
Row
Link 2
Link 3
Offset
Ө
a
1.4
4
1
45°
b
3
8
2
-30°
C
5
20
-5
225°
03
slider axis
B
X
offset
Link 2
A
R3
Link 3
R4
04
R2
02
R1
d
Figure 1.
X
4. Two links made of heat treated 6061 aluminum (Sy = 276 MPa, Sys = 160 MPa) are pinned
together using a steel dowel pin (Sy = 1398 MPa, Sys = 806 MPa) as shown below. The
links are to support a load P with a factor of safety of at least 2.0. Determine if the link will
fail first by tearout, direct shear of the pin, bearing stress on the link, or tensile stress at
section AA. (Hint: find the load P for each case and choose the case that gives the smallest
load.)
P
8 mm
P
8 mm
¡+A
3 mm
→A
10 mm
P
1. For a feature other than a sphere, circularity is where:
A. The axis is a straight line
B. The modifier is specified with a size dimension
C. All points of the surface intersected by any plane
perpendicular to an axis or spine (curved line) are
equidistant from that axis or spine
D. All points of the surface intersected by any plane
passing through a common center are equidistant
from that center
2. What type of variation is limited by a circularity toler-
ance zone?
A. Ovality
B. Tapering
C. Bending
D. Warping
3. How does the Rule #1 boundary affect the application
of a circularity tolerance?
A. The modifier must be used.
B. The feature control frame must be placed next to
the size dimension.
C. The circularity tolerance value must be less than
the limits of size tolerance.
D. Circularity cannot be applied where a Rule #1
boundary exists.
4. A circularity tolerance may use a
modifier.
A. Ø
B. F
C. M
D. ℗
5. A real-world application for a circularity tolerance is:
A. Assembly (i.e.,…
Chapter 9 Solutions
Fox And Mcdonald's Introduction To Fluid Mechanics
Java How to Program, Early Objects (11th Edition) (Deitel: How to Program)
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