GATE Flight Mechanics & Space Dynamics: Static stability: stability and control derivatives, longitudinal, directional and lateral stability, hinge moments and stick forces – Previous Year Questions
11 GATE previous year questions on Static stability: stability and control derivatives, longitudinal, directional and lateral stability, hinge moments and stick forces (Flight Mechanics & Space Dynamics, Aerospace Engineering) with answers and explanations, from every paper.
- GATE 2021 AE Q23 – The shown pitching-moment coefficient versus angle-of-attack plot indicates
- GATE 2021 AE Q34 – A twin-engine airplane at 100 m/s and density 1.225 kg/m³ has S=50 m², b=10 m, engine thrust 8000 N and lateral engine arm 5 m. Right engine fails.…
- GATE 2021 AE Q46 – Which static-stability statements are correct?
- GATE 2021 AE Q65 – An aircraft has wing area 350 m², chord 9 m, wing lift slope 0.1 per degree, CG at 30% chord and wing aerodynamic center at 25% chord. Tail area is 80…
- GATE 2022 AE Q19 – Regarding the horizontal tail of a conventional airplane, which one of the following statements is true?
- GATE 2023 AE Q19 – For a longitudinally statically stable aircraft, which one of the following represents the relationship between the coefficient of pitching moment…
- GATE 2026 AE Q23 – Which of the following statements is/are TRUE about the stability of an aircraft?
- GATE 2025 AE Q23 – For a general aviation airplane, which one of the following has a destabilizing effect on its static roll stability?
- GATE 2025 AE Q25 – To achieve longitudinal static stability of a general aviation airplane, which one of the following conditions should be satisfied?
- GATE 2025 AE Q38 – A general aviation airplane is initially in steady and level flight. The stability coefficient C m q (C m is the airplane pitching moment coefficient…
- GATE 2024 AE Q48 – For an airplane having directional / weathercock static stability, which of the following options is/are correct? (B) The variation of yawing moment…