skip to content
Lift and drag characteristics of the Douglas D-558-II research airplane obtained in exploratory flights to a Mach number of 2.0
Author:
Nugent, Jack
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54F03
Link:
https://digital.library.unt.edu/ark:/67531/metadc60393/
< New search