Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) V : aerodynamic load distributions for a series of four boattailed bodies

Author: Moskowitz, Barry
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E54B11
Link: https://digital.library.unt.edu/ark:/67531/metadc60316/

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