Experimental Droplet Impingement on Several Two-Dimensional Airfoils with Thickness Ratios of 6 to 16 Percent

Author:	Gelder, Thomas F.
Additional Authors:	Smyers, William H., Jr.
Year:	1956
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3839
Link:	https://digital.library.unt.edu/ark:/67531/metadc53503/