skip to content
Effects of nose angle and Mach number on transition on cones at supersonic speeds
Author:
Czarnecki, K R
Year:
1958
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-4388
Link:
https://digital.library.unt.edu/ark:/67531/metadc57499/
< New search