Question:
The aerodynamic center on the aerofoil is the point where
The aerodynamic center on the aerofoil is the point where
Show Hint
For subsonic aerofoils, the aerodynamic center is typically at the quarter chord.
Updated On: June 02, 2025
- pitching moment is equal to zero
- pitching moment is independent of the angle of attack
- the lift is independent of the angle of attack
- the pressure derivative becomes zero
Hide Solution
Verified By Collegedunia
The Correct Option is B
Solution and Explanation
At the aerodynamic center, the pitching moment does not change with angle of attack.
Was this answer helpful?
0
0
Top Questions on Aerodynamics
- The velocity induced at a point \(P\) by the semi-infinite vortex filament is
- According to Kutta condition, if the trailing edge is cusped, then the velocities leaving the top (\(V_1\)) and bottom (\(V_2\)) surfaces at the trailing edge should be
- In thin airfoil theory the lift curve slope is usually considered as
- The amount of lift generated in the non-rotating flow over a circular cylinder is
- Kutta-Joukowski’s theorem is defined for
View More Questions
Questions Asked in TS PGECET exam
- Melting rates of electrodes in manual metal arc welding process is mainly governed by the
- TS PGECET - 2024
- Manufacturing Processes
- The maximum area of a rectangle that can be inscribed in a circle of radius $R$ is
- TS PGECET - 2024
- 3D Geometry
- For the matrix \[ \begin{bmatrix} 2 & 1 & 1 \\ 0 & 2 & 1 \\ 1 & 0 & 1 \end{bmatrix}, \] an Eigen vector among the following vectors is
- TS PGECET - 2024
- Linear Algebra
- Which of the following expression is a tautology?
- TS PGECET - 2024
- Digital Logic
- The 2’s complement representation of the decimal value $-15$ is
- TS PGECET - 2024
- Digital Logic
View More Questions
