1.2 - 1.4 Flashcards

1
Q

In the standard atmosphere, the temperature range is considered to be _____.

A

Linear

Pg. 11

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2
Q

The negative of the temperature gradient is commonly referred to as the _____.

A

Lapse rate

Pg. 11

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3
Q

What is the definition of “geometric altitude?”

A

The altitude measured from mean sea level and measured in units of length.

Wikipedia

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4
Q

What is the definition of “geopotential altitude?”

A

The geopotential altitude is the geometric altitude corrected for variations in gravity.

Wikipedia

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5
Q

What does the Reynolds number describe?

A

A measure of the relative magnitude of the pressure forces in relation to the viscous shear forces.

Pg. 14

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6
Q

Outside the boundary layer, shear forces are _____.

A

Negligible.

Pg. 14

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7
Q

The pressure gradient across the boundary layer is _____, due to _____.

A
  1. Insignificant
  2. The very thin nature of the boundary layer.

Pg. 14

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8
Q

For high Reynolds number flows, the viscous shear forces are _____ compared to ______ forces.

A

Small
Pressure

Pg. 15

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9
Q

True or False
For flow at high Reynolds numbers, the pressure forces acting on a body can be closely approximated from an inviscid flow analysis, outside the boundary layer.

A

True

Pg. 15

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10
Q

True or False

For 2D flow over streamlined bodies, at high RE and low AOA, pressure forces contribute significantly to drag.

A

False, pressure forces do not contribute a significant amount of drag under these conditions.

Pg. 15

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11
Q

When do pressure forces dominate the drag?

A

When boundary layer seperation occurs.

Pg. 15

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12
Q

Boundary layer separation is commonly referred to as a _____.

A

Stall

Pg. 15

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13
Q

Pressure forces acting on an aircraft at high RE can be closely estimated from what type of analysis?

A

Inviscid analysis (outside the boundary layer).

Pg. 15

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14
Q

The curl of the velocity vector is typically called the _____.

A

Vorticity

Pg. 16

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15
Q

True or False

Vorticity cannot be generated in an inviscid flow.

A

True

Pg. 16

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16
Q

Vorticity far upstream is assumed _____.

A

Zero

Pg. 16

17
Q

For inviscid, irrotational flow, the continuity and momentum equations are set equal to ____.

A

Zero

Pg. 17

18
Q

True or False
For any irrotational flow, the velocity vector field can always be expressed as the gradient of a scaler potential field.

A

True

Pg. 20

19
Q

The only requirement for a potential flow is that ____.

A

The flow is irrotational.

Pg. 20

20
Q

Every potential flow is ______ flow.

A

An irrotational flow.

Pg. 20