問題一覧
1
Elevator.
2
Outboard ailerons.
3
Leading-edge flaps.
4
Low-speed and high-speed flight.
5
Low-speed flight only.
6
Aerodynamic loads on the outboard ailerons tend to twist the wingtips at high speeds.
7
Move the flight controls in the event of manual reversion.
8
Modify the downward tail load for various airpseeds in flight eliminating flight-control pressures.
9
Remains fixed for all positions.
10
Reduce control forces by deflecting in the proper direction to move a primary flight control.
11
Opposite direction.
12
Prevent a control surface from moving to a full-deflection position due to aerodynamic forces.
13
Same direction.
14
lift at low speeds.
15
Increase the camber of the wing.
16
Prevent flow separation.
17
Changes the stalling angle of attack to a higher angle.
18
Increase lift at relative slow speeds.
19
Direct air from the high-pressure area under the leading edge along the top of the wing.
20
Reduce lift without increasing airspeed.
21
Reduce the wings' lift upon landing.
22
Reduce the wings' lift upon landing.
23
four times greater.
24
A higher true airspeed for any given angle of attack.
25
A lower angle of attack.
26
lift, airspeed, and drag.
27
Drag increases becuase of increased induced drag.
28
Maximum range and distance glide.
29
An increased in induced drag requiring a higher angle of attack.
30
Induced drag increases more than parasite drag.
31
Reduce the drag caused by supersonic flow over portions of the wing.
32
Weight, load factor, and power.
33
An abrupt change in relative wind.
34
making the wing surface rough and/or directing high pressure air over the top of the wing or flap through slots.
35
Lift divided by the total weight.
36
3 G's.
37
is constant.
38
Angle of bank.
39
Both total lift force and load factor increase.
40
1,948.0 pounds.
41
6,767.8 pounds.
42
8,290.8 pounds.
43
1302.8 pounds.
44
1,663.2 pounds.
45
924.5 pounds.
46
914.1 pounds.
47
681.6 pounds.
48
1,245.3 pounds.
49
1,611.6 pounds.
50
857.1 pounds.
51
25,721.9 pounds.
52
21,769.9 pounds.
53
21,669.8 pounds.
54
12,262.4 pounds.
55
9,681.5 pounds.
56
183 lb/sq ft.
57
115 lb/sq ft.
58
144 lb/sq ft.
59
76 lb/sq ft.
60
176 lb/sq ft.
61
183 lb/sq ft.
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
Via · 78問 · 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
78問 • 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
Via · 81問 · 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
81問 • 1年前CPL Radio Telephony (1)
CPL Radio Telephony (1)
Via · 100問 · 1年前CPL Radio Telephony (1)
CPL Radio Telephony (1)
100問 • 1年前CPL Radio Telephony (2)
CPL Radio Telephony (2)
Via · 100問 · 1年前CPL Radio Telephony (2)
CPL Radio Telephony (2)
100問 • 1年前CPL Radio Telephony (3)
CPL Radio Telephony (3)
Via · 20問 · 1年前CPL Radio Telephony (3)
CPL Radio Telephony (3)
20問 • 1年前Met 1
Met 1
Via · 78問 · 1年前Met 1
Met 1
78問 • 1年前Met 2
Met 2
Via · 43問 · 1年前Met 2
Met 2
43問 • 1年前Met 3
Met 3
Via · 49問 · 1年前Met 3
Met 3
49問 • 1年前Met 4
Met 4
Via · 14問 · 1年前Met 4
Met 4
14問 • 1年前Met 5
Met 5
Via · 83問 · 1年前Met 5
Met 5
83問 • 1年前Met 6
Met 6
Via · 35問 · 1年前Met 6
Met 6
35問 • 1年前Met 7
Met 7
Via · 54問 · 1年前Met 7
Met 7
54問 • 1年前Met 8
Met 8
Via · 7問 · 1年前Met 8
Met 8
7問 • 1年前Human Performance 3
Human Performance 3
Via · 57問 · 1年前Human Performance 3
Human Performance 3
57問 • 1年前Met 9
Met 9
Via · 35問 · 1年前Met 9
Met 9
35問 • 1年前Met 10
Met 10
Via · 43問 · 1年前Met 10
Met 10
43問 • 1年前AGK 1
AGK 1
Via · 63問 · 1年前AGK 1
AGK 1
63問 • 1年前AGK 2
AGK 2
Via · 47問 · 1年前AGK 2
AGK 2
47問 • 1年前AGK 3
AGK 3
Via · 97問 · 1年前AGK 3
AGK 3
97問 • 1年前問題一覧
1
Elevator.
2
Outboard ailerons.
3
Leading-edge flaps.
4
Low-speed and high-speed flight.
5
Low-speed flight only.
6
Aerodynamic loads on the outboard ailerons tend to twist the wingtips at high speeds.
7
Move the flight controls in the event of manual reversion.
8
Modify the downward tail load for various airpseeds in flight eliminating flight-control pressures.
9
Remains fixed for all positions.
10
Reduce control forces by deflecting in the proper direction to move a primary flight control.
11
Opposite direction.
12
Prevent a control surface from moving to a full-deflection position due to aerodynamic forces.
13
Same direction.
14
lift at low speeds.
15
Increase the camber of the wing.
16
Prevent flow separation.
17
Changes the stalling angle of attack to a higher angle.
18
Increase lift at relative slow speeds.
19
Direct air from the high-pressure area under the leading edge along the top of the wing.
20
Reduce lift without increasing airspeed.
21
Reduce the wings' lift upon landing.
22
Reduce the wings' lift upon landing.
23
four times greater.
24
A higher true airspeed for any given angle of attack.
25
A lower angle of attack.
26
lift, airspeed, and drag.
27
Drag increases becuase of increased induced drag.
28
Maximum range and distance glide.
29
An increased in induced drag requiring a higher angle of attack.
30
Induced drag increases more than parasite drag.
31
Reduce the drag caused by supersonic flow over portions of the wing.
32
Weight, load factor, and power.
33
An abrupt change in relative wind.
34
making the wing surface rough and/or directing high pressure air over the top of the wing or flap through slots.
35
Lift divided by the total weight.
36
3 G's.
37
is constant.
38
Angle of bank.
39
Both total lift force and load factor increase.
40
1,948.0 pounds.
41
6,767.8 pounds.
42
8,290.8 pounds.
43
1302.8 pounds.
44
1,663.2 pounds.
45
924.5 pounds.
46
914.1 pounds.
47
681.6 pounds.
48
1,245.3 pounds.
49
1,611.6 pounds.
50
857.1 pounds.
51
25,721.9 pounds.
52
21,769.9 pounds.
53
21,669.8 pounds.
54
12,262.4 pounds.
55
9,681.5 pounds.
56
183 lb/sq ft.
57
115 lb/sq ft.
58
144 lb/sq ft.
59
76 lb/sq ft.
60
176 lb/sq ft.
61
183 lb/sq ft.