Chapter 7 Flashcards

(55 cards)

1
Q

Define a perfect gas.

A

A gas in which the intermolecular forces are neglected.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

The energy of a given molecule is the sum of what?

A

It’s transnational, rotational, vibrational, and electronic energies.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

The sum of the energies of all the molecules in a given volume of gas is defined as the ____.

A

Internal energy of the gas.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

The internal energy per unit mass is defined by what variable?

A

Entropy – e

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

For a perfect gas, both e and h are functions of ____. only.

A

Temperature

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

When temperatures are below _____K the specific heats are usually ____.

A

1000K

constant.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

What is a “Calorically Perfect” gas?

A

As gas in which the two specific heats (cp and cv) are constant.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Define an Adiabatic Process.

A

One in which no heat is added to or taken away from the system.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Define a Reversible Process.

A

One in which no dissipative phenomena occur, this is, where the effects of viscosity, thermal conductivity, and mass diffusion are absent.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Defin Isentropic process.

A

One that is both adiabatic and reversible.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What are the three main dissipative phenomena?

A
  1. Viscosity
  2. Thermal Conductivity
  3. Mass diffusion
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Explain why many practical flows can be modeled as isentropic?

A

The viscous boundary layer adjacent to the surface is thin compared with the entire flow field, and hence large regions of the flow can be assumed isentropic.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Entropy is a function of what two variables?

A

Temperature and pressure.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

True or False

Entropy increases with increasing temperature.

A

True.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

True or False

Entropy decreases with increasing temperature.

A

False, it decreases with decreasing temperature.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

How does pressure affect entropy?

A

As pressure increases, entropy decreases and VV.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Incompressible flows obey ____ laws.

A

Mechanical Laws

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

What are the primary dependant variables for compressible flow?

A

p, V, rho, e, and T

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Is Bernoulli’s equation valid for compressible flow?

A

No

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

What is static pressure?

A

The measure of the purely random motion of molecules in a gas.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

What is stagnation pressure?

A

The pressure existing at a point (or points) in the flow where V=0.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

What is the total temperature?

Note: Define it conceptually

A

If a fluid element is adiabatically slowed to zero velocity the temperature of the fluid element will change. At the point of zero velocity, the temp of the fluid element is the total temperature.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

What is total enthalpy?

Note: Define it conceptually

A

If a fluid element is adiabatically slowed to zero velocity the temperature of the fluid element will change. At the point of zero velocity, the temp of the fluid element is the total temperature. The total enthalpy is the total temperature multiplied by cp.

24
Q

True or False

Total enthalpy is constant along a streamline.

25
Total pressure and total density are related to what process?
An Isentropic process/flow.
26
Conceptually define specific heat.
The energy required to raise the temperature of a unit mass of a substance by one unit degree. TD Textbook
27
What is the difference between cp and cv?
cv represents the energy required to raise the temperature of the unit mass of a substance by one degree as the volume is maintained constant. The energy required to do the same thing as the pressure is maintained constant is the specific heat at a constant pressure (cp). TD Textbook
28
How are the magnitudes of cp and cv related?
cp > cv
29
True or False The specific heat at a constant volume (cv) is related to the changes in internal energy, and the specific heat at constant pressure (cp) to the changes in enthalpy.
True TD Textbook
30
What is the variable cv named?
Specific heat at a constant volume.
31
What is the variable cp named?
Specific heat at a constant pressure.
32
What is a shockwave?
A shock wave is an extremely thin region, typically on the order of 10^−5 cm, across which the flow properties can change drastically.
33
True or False | Flow across a shockwave is adiabatic.
True
34
The pressure, density, temperature, and entropy_____ across a shockwave.
Increase
35
Mach number and velocity ____ across a shockwave.
Decrease
36
True or False | Subsonic flows have a smoothly varying streamline pattern.
True
37
True or False In subsonic flow, the streamline far ahead of the body is forewarned about the presence of the body and begins to adjust accordingly.
True.
38
True or False In supersonic flows, the flow upstream of the body does not know about the presence of the body until it encounters the leading edge shockwave.
True
39
True or False | Shockwaves are usually at normal angles to the flow.
False, they are usually at oblique angles to the flow.
40
Shockwaves can be considered as an ______ process.
Explosive decompression.
41
True or False | Total entropy is constant across a shockwave.
True
42
Flow ahead of a shockwave (in both the normal and oblique case) must be _____.
Supersonic (M>1).
43
True or False | In some cases behind an oblique shockwave, the flow can be sufficiently decelerated such that the flow is subsonic.
True
44
For normal shockwaves, the downstream flow is always _____.
Subsonic.
45
When a fluid is not flowing, it is at Stagnation State and its thermodynamic properties are _____.
Stagnation Properties.
46
Describe a stagnation reference state.
For a flowing fluid, A "Stagnation State" is defined as a reference estate that would exist if the fluid were decelerated to zero speed and zero potential.
47
To obtain a unique stagnation state, the deceleration process must be ______.
Adiabatic and reversible = "isentropic."
48
What instrument is usually employed to measure total temperature and total pressure?
A pitot-tube.
49
When a fluid is not flowing, its thermodynamic properties are _______.
Stagnation or total properties.
50
What is a stagnation reference state?
A reference state that would exist if the fluid were decelerated to zero speed and zero potential.
51
To obtain a unique stagnation state, the deceleration process must be ____ and _____.
Adiabatic and reversible.
52
True or False | A process does not have to be reversible for Stagnation Enthalpy and Stagnation Temperature.
True
53
True or False
Total Enthalpy and Total temperature are constant for steady and adiabatic flow.
54
For non-adiabatic flow, the temperature and Enthalpy are ____ constant.
Not
55
Irreverstibilites cause entropy to _____ and total pressure to _____.
Increase | Decrease