skip to content
Comparison of airfoil sections on two triangular-wing-fuselage configurations at transonic speeds from tests by the NACA wing-flow method
Author:
Hall, Albert W.
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51F01
Link:
https://digital.library.unt.edu/ark:/67531/metadc59009/
< New search