Aircraft Stability and Control Question
Aircraft Stability and Control Question
Aircraft Stability and Control Question
QUESTION BANK
UNIT I
PART-A
1. Define stability
2. State three modes of stability
3. Define static stability
4. Define dynamic stability
5. Difference between static stability and dynamic stability
6. What is meant by 'degree of freedom'
7. State two conditions for static longitudinal stability and indicate them
with a Plot
8. The statically stable aircraft may be dynamically stable or unstable.
Similarly dynamically stable aircraft may be statically stable or
unstable". Are both statement true
9. Write the types of axis components in aircraft
10. What is coordinate transformation
11. Tail volume ratio
PART-B
1. Derive the axis component of entire airplane
2. Derive the force and moment equation act in an aircraft
3. Explain the basic concepts of static and dynamic stability with
example
4. Explain the longitudinal static stability in detail
5. Explain the conditions of longitudinal static stability
6. Derive the equation for overall contribution of aircraft pitching
moment about c.g
7. Derive contribution of wing of aircraft pitching moment
8. Derive the contribution of tail of aircraft pitching moment
9. Explain the contribution of fuselage of aircraft pitching moment
10. Define centre of gravity, aerodynamic centre, centre of pressure
UNIT II
PART-A
UNIT III
UNIT III
PART A
PART B