Intro to Hyp. - Mid Term Review Flashcards

1
Q

Newtons 2nd law requires acceleration to be expressed in an _____ frame.

A

Inertial

Source Notes, 2.1

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2
Q

What is the physical interpretation of the ballistic coefficient?

A

Its a measure of an objects ability to overcome air resistance in flight. A higher value implies that a given object can overcome drag forces more efficiently than an object with a lower coefficient.

Dynamics of Atmospheric Re-Entry, F.J. Regan, Pg. 182

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3
Q

In regards to defining continuum vs. rarified flow, what parameter is of primary utility?

A

The Knudsen number.

Kn = λ/L

Where λ is the mean free path and L is a reference length.

Hypersonic Aerothermodynamics, J. Bertin, Pg. 12

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4
Q

For the stagnation region, what are the four dominant chemical reactions for equilibrim in order of occurrence with increasing velocity?

A
  1. Vibrational Energy Excited
  2. Oxygen Dissocates
  3. Nitrogen Dissocates
  4. Ionization of Nitrogen and Oxygen

Hypersonic Aerothermodynamics, J. Bertin, Pg. 19 (Fig. 1.14)

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5
Q

In a thermally perfect gas, the state variables e and h are determined by what parameter?

A

Absolute temperature.

Source Notes: 3.3.1

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6
Q

The specific heats begin to vary with absolute temperature for air around Mach = __________. Chemical effects begin at aroung Mach = __________.

A

M = 3
M = 6

Source Notes: 3.3.1

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7
Q

True or False:
Following a bow shock the change in entropy (ds) in the shock layer is negligible compared to the boundary layer.

A

True.

Source Notes: 3.1.2 Hypersonic Gas Dynamics

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8
Q

Generally, the continuim approach is valid for a Knudsen number Kn < _________.

A

0.01

Source Notes: 3.1.2 Hypersonic Gas Dynamics

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9
Q

What paramter discussed in class can serve as a measure of the degree of dissociation?

A

z = R_{mix}/R_{air}

Lecture: 10/31/2023

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10
Q

What is the theoretical upper bound for z, where z = R_{mix}/R_{air}?

A

z = 2.07 ~ 2

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11
Q

True or False:
Monotonic gasses only have translational degrees of freedom. There are no vibrational or rotational modes to excite.

A

True.

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12
Q

At what approximate temperature (in Kelvin) does vibrational excitation of diatomic oxygen and nitrogen begin to occur?

A

1000 - 1500 K

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13
Q

At what temperature range, does diatomic oxygen bein to dissociate?

A

Approximately 2000 - 3000 K

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14
Q

At what temperature range does diatomic nitrogen begin to dissociate?

A

Approximately 3000-4500 K

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15
Q

At what temperature (in Kelvin) does ionization generally occur for air?

A

Approximately 5000 K

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16
Q

Why does oxygen dissociation occur before nitrogen?

A

The dissociation energy for oxygen is much lower than nitrogen (498 vs. 945 kJ/mol) .

17
Q

What are the four primary “real gas effects?”

A
  1. Dissociation
  2. Ionization
  3. Chemical Reactions
  4. Vibrational Activation
18
Q

For the unmodified Newtonian model of aerodynamics, the Cp (pressure coefficient) has a max value of _____, and a specific heat ratio of _______.

A

2
1

19
Q

For modified newtonian model of aerodynamics, Cp_w < ________.

Note: Cp_w = pressure coefficient at the wall.

A

2 (which is the cp_max for the unmodified Newtonian model).

20
Q

True or False:
In the modified Newtonian model, the calculation of the pressure coefficient at the wall becomes a function of the specific heat ratio.

A

True.

21
Q

What are the three primary transport properties that need to be considered in hypersonic flows?

Give the corresponding coefficients for each as they would appear in the equations of motion.

A
  1. Mass diffusion (D for use in Fick’s law)
  2. Momentum Diffusion (μ for the dynamic viscosity)
  3. Energy Diffusion (κ for use in Fourniers equation)
22
Q

What is one of the primary constraints for hypersonic air-breathing vehicles in terms of it’s trajectory state?

A

The trajectory must be tailored such that a high dynamic pressure may be maintained. This ensures:
1. Efficient combustion
2. Effective mixing of fuel with air
3. Safe engine cooling
4. Optimal oxygen/fuel ratios

23
Q

What is the non-dimensional paramter that links the viscosity of a medium to its thermal conductivity?

A

The Prandtl number (Pr)