skip to content
The Calculation of Pressure on Slender Airplanes in Subsonic and Supersonic Flow
Author:
Heaslet, Max A.
Year:
1953
Document Type:
N/A
Series:
NACA Technical Reports
Report Number:
NACA-TR-1185
Link:
https://digital.library.unt.edu/ark:/67531/metadc65547/
< New search