skip to content
Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing
Author:
Lindsey, W. F.
Year:
1944
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-L-75, NACA-CB-L4E29
Link:
https://digital.library.unt.edu/ark:/67531/metadc62406/
< New search