For a symmetric airfoil at an angle of attack of $10^{\circ}$, assuming thin airfoil theory, the magnitude of the pitching moment coefficient about the leading edge is________ (round off to 2 decimal places).

Question ID - 155468 | SaraNextGen Top Answer

For a symmetric airfoil at an angle of attack of $10^{\circ}$, assuming thin airfoil theory, the magnitude of the pitching moment coefficient about the leading edge is________ (round off to 2 decimal places).