skip to content
Corrections for Lift, Drag, and Moment of an Airfoil in a Supersonic Tunnel Having a Given Static Pressure Gradient
Author:
Ludloff, H. F.
Year:
1952
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-2849
Link:
https://digital.library.unt.edu/ark:/67531/metadc56509/
< New search