An NACA transonic test section with tapered slots tested at Mach numbers to 1.26
NACA research memorandum ; L50B14
1950
19 S
Ill., graph. Darst
Report
English
Passive drag reduction on a complete NACA 0012 airfoil at transonic Mach numbers
Tema Archive | 1987
|NACA Transonic Wing-tunnel Test Sections
NTRS | 1948
|