skip to content
Effects of Reynolds number on the aerodynamic characteristics of a delta wing at Mach number of 2.41
Author:
Hatch, John E , Jr
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51H06
Link:
https://digital.library.unt.edu/ark:/67531/metadc58969/
< New search