Which of the following need NOT be reflected in a sketch when using the Linear Momentum Equation? a. The direction of the velocities b.Internal forces within the free body diagram c. The boundaries of the control volume d.The pressures at the control sections The following operations may be done on a dimensionless product to obtain other another product without losing its non-dimensionality EXCEPT: a.Adding it to another dimensionless product b.Multiplying it by another dimensionless product c.Impose a constant exponent on it d.Multiplying it by a constant An airplane wing, with chord length of 1.5 m and span of 9 m, is designed to move through standard air (v= 1.51x105 m²/s) at a speed of 7.5 m/s. A 1/10-scale model of this wing is to be tested in a water tunnel (v= 1.00×106 m²/s). If viscous effects govern, what speed is necessary in the water tunnel to achieve dynamic similarity? a.11.33 m/s b.4.97 m/s c.1.51 m/s d.2.98 m/s

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Which of the following need NOT be reflected in a sketch when using the Linear Momentum
Equation?
a. The direction of the velocities
b.Internal forces within the free body diagram
c. The boundaries of the control volume
d. The pressures at the control sections
The following operations may be done on a dimensionless product to obtain other another
product without losing its non-dimensionality EXCEPT:
a.Adding it to another dimensionless product
b.Multiplying it by another dimensionless product
c.Impose a constant exponent on it
d. Multiplying it by a constant
An airplane wing, with chord length of 1.5 m and span of 9 m, is designed to move through
standard air (v= 1.51×105 m²/s) at a speed of 7.5 m/s. A 1/10-scale model of this wing is to
be tested in a water tunnel (v= 1.00×106 m²/s). If viscous effects govern, what speed is
necessary in the water tunnel to achieve dynamic similarity?
a.11.33 m/s
b.4.97 m/s
c.1.51 m/s
d.2.98 m/s
A dam spillway is to be tested with a 1:20 scale model. The model flow has an average
velocity of 0.75 m/s and a volume flow of 0.06 cms. If the measured force on a certain part
of the model is 1.5 N, what will be the corresponding force on the prototype be?
a. 1,200 N
b.12,000 N
c.600 N
d.6,000 N
Transcribed Image Text:Which of the following need NOT be reflected in a sketch when using the Linear Momentum Equation? a. The direction of the velocities b.Internal forces within the free body diagram c. The boundaries of the control volume d. The pressures at the control sections The following operations may be done on a dimensionless product to obtain other another product without losing its non-dimensionality EXCEPT: a.Adding it to another dimensionless product b.Multiplying it by another dimensionless product c.Impose a constant exponent on it d. Multiplying it by a constant An airplane wing, with chord length of 1.5 m and span of 9 m, is designed to move through standard air (v= 1.51×105 m²/s) at a speed of 7.5 m/s. A 1/10-scale model of this wing is to be tested in a water tunnel (v= 1.00×106 m²/s). If viscous effects govern, what speed is necessary in the water tunnel to achieve dynamic similarity? a.11.33 m/s b.4.97 m/s c.1.51 m/s d.2.98 m/s A dam spillway is to be tested with a 1:20 scale model. The model flow has an average velocity of 0.75 m/s and a volume flow of 0.06 cms. If the measured force on a certain part of the model is 1.5 N, what will be the corresponding force on the prototype be? a. 1,200 N b.12,000 N c.600 N d.6,000 N
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