Aerodynamic Forces and Moments on a Large Ogive-Cylinder Store at Various Locations Below the Fuselage Center Line of a Swept-Wing Bomber Configuration at a Mach Number of 1.61

Author: Morris, Odell A.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56I25
Link: https://digital.library.unt.edu/ark:/67531/metadc52977/

< New search