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 :-

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).

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