Experimental investigation of the flow around lifting symmetrical double-wedge airfoils at Mach numbers of 1.30 and 1.41

Author: Gooderum, Paul B.
Year: 1956
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3626
Link: https://digital.library.unt.edu/ark:/67531/metadc57890/

< New search