Determination of indicial lift and moment of a two-dimensional pitching airfoil at subsonic mach numbers from oscillatory coefficients with numerical calculations for a Mach number of 0.7

Author:	Mazelsky, Bernard
Year:	1952
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2613
Link:	https://digital.library.unt.edu/ark:/67531/metadc56169/