skip to content
Maintaining Laminar Flow in the Boundary Layer Using a Swept-Back Wing
Author:
Brennecke
Year:
1948
Document Type:
N/A
Series:
NACA Technical Memorandums
Report Number:
NACA-TM-1180
Link:
https://digital.library.unt.edu/ark:/67531/metadc64820/
< New search