skip to content
Calculated spanwise lift distributions and aerodynamic influence coefficients for swept wings in subsonic flow
Author:
Diederich, Franklin W.
Year:
1955
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3476
Link:
https://digital.library.unt.edu/ark:/67531/metadc57721/
< New search