Numerical Determination of Indicial Lift of a Two-Dimensional Sinking Airfoil at Subsonic Mach Numbers From Oscillatory Lift Coefficients With Calculations for Mach Number 0.7

Author:	Mazelsky, Bernard
Year:	1951
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2562
Link:	https://digital.library.unt.edu/ark:/67531/metadc55897/