大学MOOC Airplane Stability and Control(Northwestern Polytechnical University)1458073162 最新慕课完整章节测试答案
1. Introduction, Basic Concepts and Definitions
文章目录
- 1. Introduction, Basic Concepts and Definitions
- 10. Typical Modes
- 2. Longitudinal Static Stability Contributions
- 3. Longitudinal Control and Trim
- 4. Control Force and Stability in Maneuver Flight
- 5. CG Limits and Directional Static Stability
- 6. Directional Stability Contributions and Control Surfaces
- 7. Lateral Stability, Criterion and Control
- 8. Equations of Motion
- 9. Eigenvalue and Dynamic Stability
Quiz 1
1、单选题:
The AOA response of an aircraft after being disturbed is given below. The airplane is statically , and dynamically .
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选项:
A: stable, stable
B: stable, unstable
C: unstable, stable
D: unstable, unstable
答案: 【 stable, unstable】
2、单选题:
For the International Coordinate System, x-axis points from CG to the nose, and y-axis points from CG to the right. According to the right-hand system, the z-axis points downward. For the USSR coordinate system, x-axis points from CG to the nose, and y-axis points upward. According to the right-hand system, the z-axis points .
选项:
A: upward
B: downward
C: to the left
D: to the right
答案: 【 to the right】
3、单选题:
The average Cooper-Harper rating of an aircraft is 4.5, it belongs to flying quality.
选项:
A: Level I
B: Level II
C: Level III
D: Uncontrollable
答案: 【 Level II】
4、单选题:
According to the sign convention in this course (international coordinate system), roll to the right about the x-axis is , and yaw to the left about the z-axis is .
选项:
A: positive, positive
B: negative, positive
C: positive, negative
D: negative, negative
答案: 【 positive, negative】
5、单选题:
If the side force acting on the rudder is left (negative), this side force will generate a yawing moment.
选项:
A: left
B: right
C: upward
D: downward
答案: 【 right】
6、单选题:
Rudder locates aft of CG, therefore, a left rudder force will generate a right yawing moment.If the lift acting on the horizontal tail is upward (positive), this tail lift will generate a pitching moment.
选项:
A: nose-up
B: nose-down
C: right
D: left
答案: 【 nose-down】
7、单选题:
Which category of flight phases has the highest flying quality requirement?
选项:
A: Category A
B: Category B
C: Category C
D: Category D
答案: 【 Category A】
8、多选题:
Which of the following aircraft belong to class IV?
选项:
A: F-22
B: A-10
C: C-130
D: B-2
E: A320
F: F/A-18
答案: 【 F-22;
A-10;
F/A-18】
9、多选题:
Which flight phases belong to Category A?
选项:
A: Takeoff
B: Landing
C: Air-to-Air Combat
D: Formation
E: Cruise
F: Aerobatic
答案: 【 Air-to-Air Combat;
Formation;
Aerobatic】
10、判断题:
According to the Cm ~ CL figure, the aircraft is longitudinally stable before stall.
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选项:
A: 正确
B: 错误
答案: 【 正确】
11、判断题:
and
are the same coefficient.
选项:
A: 正确
B: 错误
答案: 【 错误】
10. Typical Modes
Quiz 10
1、单选题:
At low speeds, the phugoid frequency with the increase of forward velocity.
选项:
A: decreases
B: increases
C: remains unchanged
D: [ / ]
答案: 【 decreases】
2、单选题:
The eigenvalue of roll-subsidence mode mainly depends on which of the following parameters.
选项:
A: 
B: 
C: 
D: 
答案: 【 
】
3、单选题:
The Dutch-roll frequency mainly depends on which of the following parameters.
选项:
A: 
B: 
C: 
D: 
答案: 【
】
4、单选题:
When the aircraft roll to the right, the right wing AOA will .
选项:
A: increase
B: decrease
C: remain unchanged
D: [ / ]
答案: 【 increase】
5、单选题:
If the spiral mode eigenvalue is negative, theflying quality is .
选项:
A: Level I
B: Level I
C: Level II
D: Uncontrollable
答案: 【 Level I】
6、多选题:
Which of the following parameters are related to the Dutch-roll mode characteristics?
选项:
A: 
B: 
C: 
D: 
E: 
F: 
答案: 【 
;
;
;
】
7、多选题:
Which of the following situations satisfy the Level I flying quality requirements?
选项:
A: Fighter at Cat A flight phase, Tr = 1.2
B: Fighter at Cat B flight phase, Tr = 1.2
C: Fighter at Cat C flight phase, Tr = 1.2
D: Cargo at Cat B flight phase, Tr = 1.2
E: Cargo at Cat C flight phase, Tr = 1.2
答案: 【 Fighter at Cat B flight phase, Tr = 1.2;
Cargo at Cat B flight phase, Tr = 1.2;
Cargo at Cat C flight phase, Tr = 1.2】
8、判断题:
For the spiral mode, the requirements for Category A is higher than those for Category B and C.
选项:
A: 正确
B: 错误
答案: 【 错误】
9、判断题:
The roll-subsidence mode characteristics of high AR aircraft are better than low AR aircraft.
选项:
A: 正确
B: 错误
答案: 【 正确】
