skip to content
Longitudinal Stability and Control Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds From Tests by the NACA Wing-Flow Method
Author:
Silsby, Norman S.
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L8G30
Link:
https://digital.library.unt.edu/ark:/67531/metadc57937/
< New search