問題一覧
1
Temperature is a measure of the kinetic energy of the molecules of any substance
2
Directly with pressure
3
6,000 pounds
4
Relative humidity
5
Positive air pressure below the wing’s surface and negative air pressure above the wing’s surface along with the downward deflection of air.
6
Be reduced to one half its original value
7
Asymmetrical lateral control at a near stall angles of attack
8
Remain the same
9
High temperature with high humidity
10
Everybody persists in its state of rest, or of motion in a straight line, unless acted upon by some force.
11
Diffusion
12
35 parts of dry air and 65 parts of water vapor
13
Wingspan to the mean chord
14
Unmetered pressure, 17 PSI; metered pressure, 5 PSI; atmospheric pressure, 14.7 PSI
15
Absolute humidity
16
1,2 and 3
17
Ambient temperature
18
Increase the lift to drag ratio
19
8000 pounds
20
Not change
21
Ensure that the wing root areas stall first
22
A low stall speed
23
360 foot-pounds
24
40 pounds
25
Dew point
26
The actual amount of the water vapor in a mixture of air and water.
27
Increase lateral stability
28
Changes with a change in temperature
29
840 foot pounds
airlaw
airlaw
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new set
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human factor
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human factor
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human factor 2
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29問 • 1年前Engine instrument system
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54問 • 1年前Propellers
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Propellers (2)
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Induction and engine airflow system
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Induction and engine airflow system
42問 • 1年前Ignition starting system
Ignition starting system
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Ignition starting system (2)
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Ignition starting system (2)
29問 • 1年前Auxiliary power unit
Auxiliary power unit
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10問 • 1年前Reciprocating engines
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Reciprocating engines
100問 • 1年前Turbine engines
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ユーザ名非公開 · 20問 · 1年前Turbine engines (2)
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20問 • 1年前Fuel metering systems
Fuel metering systems
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Aircraft landing gear system
79問 • 1年前Sheetmetal & Non sheetmetalic structure
Sheetmetal & Non sheetmetalic structure
ユーザ名非公開 · 100問 · 1年前Sheetmetal & Non sheetmetalic structure
Sheetmetal & Non sheetmetalic structure
100問 • 1年前Sheetmetal and non sheetmetalic structure
Sheetmetal and non sheetmetalic structure
ユーザ名非公開 · 30問 · 1年前Sheetmetal and non sheetmetalic structure
Sheetmetal and non sheetmetalic structure
30問 • 1年前Aircraft fuel system
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ユーザ名非公開 · 100問 · 1年前Aircraft fuel system
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100問 • 1年前問題一覧
1
Temperature is a measure of the kinetic energy of the molecules of any substance
2
Directly with pressure
3
6,000 pounds
4
Relative humidity
5
Positive air pressure below the wing’s surface and negative air pressure above the wing’s surface along with the downward deflection of air.
6
Be reduced to one half its original value
7
Asymmetrical lateral control at a near stall angles of attack
8
Remain the same
9
High temperature with high humidity
10
Everybody persists in its state of rest, or of motion in a straight line, unless acted upon by some force.
11
Diffusion
12
35 parts of dry air and 65 parts of water vapor
13
Wingspan to the mean chord
14
Unmetered pressure, 17 PSI; metered pressure, 5 PSI; atmospheric pressure, 14.7 PSI
15
Absolute humidity
16
1,2 and 3
17
Ambient temperature
18
Increase the lift to drag ratio
19
8000 pounds
20
Not change
21
Ensure that the wing root areas stall first
22
A low stall speed
23
360 foot-pounds
24
40 pounds
25
Dew point
26
The actual amount of the water vapor in a mixture of air and water.
27
Increase lateral stability
28
Changes with a change in temperature
29
840 foot pounds