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

Morris, Odell A
naca-rm-l56i25
January 14, 1957


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-l56i25.pdf