skip to content
Longitudinal Stability and Control Characteristics of a Semispan Airplane Model With a Sweptback Wing and Tail From Tests at Transonic Speeds by the NACA Wing-Flow Method
Author:
Sawyer, Richard H.
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L8B19
Link:
https://digital.library.unt.edu/ark:/67531/metadc57580/
< New search