General solutions for flow past slender cambered wings with swept trailing edges and calculation of additional loading due to control surfaces

Author:	Klunker, E. B.
Year:	1958
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-4242
Link:	https://digital.library.unt.edu/ark:/67531/metadc57328/