The zero-lift drag of a slender body of revolution (NACA RM-10 research model) as determined from tests in several wind tunnels and in flight at supersonic speeds

Author: Evans, Albert J
Year: 1953
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2944
Link: https://digital.library.unt.edu/ark:/67531/metadc56732/

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