Test 3 Concept Questions Flashcards

1
Q

What does steady flow mean in terms of energy conservation?

A

The rate of change of energy within a CV is equal to 0.

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2
Q

What do we need “alpha (a)” for and how is it calculated?

A

Alpha is the kinetic energy flux coefficient and is used to convert u^3 to v^3 or non-uniform velocity in to uniform velocity. It is calculated by the (intgral over the area of u^3)/(V^3*A)

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3
Q

What is the physical meaning of the terms of the energy equation?

A
P/pg = Rate at which work is done on the control volume
z = rate at which potential energy is gained/lost by CV
av^2/2g = rate at which KE is entering/leaving CV
hL = Rate of energy loss in CV
ht = Rate of energy that is provided to the turbine by the flow
hp = Rate at which energy is provided to flow by the pump
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4
Q

How do you convert the quantity of a given head into power and vice versa?

A

To convert head to power multiply head by “pgQ”

To convert power to head divide power by “pgQ”

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5
Q

What do the energy and hydraulic grade lines represent?

A
HGL = P/pg + z
EGL = P/pg + z + av^2/2g
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6
Q

What term in the energy equation represents a change in heat/internal energy?

A

hL = Head Loss

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7
Q

Why is dimensional analysis important?

A

By grouping the variables pertinent to a study into dimensionless groups, we can extract max information from a minimum number of experiments or tests. It also provides meaningful results and a better understanding of the flow behavior.

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8
Q

What are the primary dimensions?

A

M,L,T

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9
Q

What are the rules for selecting repeating variables?

A

Nr <= Nd Nr = Nd
Repeating Variables must not form a dimensionless group
Do not choose the variable being investigated as a repeating variable

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10
Q

What is similitude and how do we achieve it?

A

The theory that allows us to predict the behavior of the prototype based on a geometric, kinematic, and dynamically similar model.

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11
Q

Knowledge of Reynolds number, Froude’s Number, Weber’s Number, and Machs Number?

A
Re = pvL/u = Fi/Fv
Fr = V/sqrt(gL) = Fi/Fg
Weber = sigma/v^2Lp = Fi/Fsigma
Mach = V/sqrt(E/p) = Fi/Fe
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12
Q

Expressions for inertial, viscous, gravity, elastic, and surface tension in forces?

A
Inertial = pV^2L^2
Viscous = uVL
Gravity = pgL^3
Elastic = EL^2
Surface = sigma(L)
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13
Q

How do we achieve geometrical, dynamic, and kinematic similarities.

A

Geometric = Same shape
Dynamic = Rep = Rem
= Fp = Fm
If geometric and dynamic are satisfied so is kinematic.

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14
Q

What is the Boundary Layer?

A

A zone close to a solid surface where velocity is less than Uo.

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15
Q

How does the wall shear stress vary along the length of a plate in a typical BL?

A

Look at the chart in notes

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16
Q

What is the difference between laminar and turbulent flow?

A

Laminar Flow = Particles move in layers without mixing

Turbulent Flow = Fluid particles move haphazardly in all directions

17
Q

When does the LBL turn into a TBL?

A

When Re > 500,000 (Leading Edge)

When Re > 3000 (Pipe)

18
Q

Which type of flow is more conducive for mixing?

A

Turbulent

19
Q

The difference between the laminar and turbulent velocity profiles

A

Look at chart in notes.

20
Q

Which type of boundary layer grows faster?

A

Turbulent grows much faster.

21
Q

What are the components of Drag Force?

A

Total Drag Force = Friction Drag + Form Drag

22
Q

For Cylinders and spheres what causes a sudden reduction in the drag coefficient?

A

A sudden reduction in Cd is associated with LBC changing to TBC

23
Q

LBC

A

Laminar Boundary Condition

24
Q

TBC

A

Turbulent Boundary Condition

25
Q

Under what condition is the drag coefficient for cylinders and spheres independent of Re?

A

When the total drag is made up of form dray only. When friction drag’s contribution to the total drag is negligible

26
Q

For bodies with sharp edges, why is Cd mostly independent of Re

A

Because flow separation points are determined by the geometry of the body. The flow always separates at the same point independent of Re.