skip to content
Free-flight investigation to obtain drag-at-lift and stability data for a 60 degree delta-wing-body configuration over a Mach number range of 1.3 to 1.6
Author:
Welsh, Clement J
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55G14
Link:
https://digital.library.unt.edu/ark:/67531/metadc61582/
< New search