Effect of Mach and Reynolds Numbers on the Maximum Lift Coefficient Obtainable in Gradual and Abrupt Stalls of a Pursuit Airplane Equipped With a Low-Drag Wing

Author:	Spreiter, John R.
Additional Authors:	Galster, George M.
Year:	1945
Document Type:	N/A
Series:	NACA Wartime Reports
Report Number:	NACA-WR-A-5, NACA-MR-A5G06
Link:	https://digital.library.unt.edu/ark:/67531/metadc61288/