Flight investigation at Mach numbers from 0.8 to 1.4 to determine the zero-lift drag of wings with 'M' and 'W' plan forms

Katz, Ellis Marley, Edward T Pepper, William B
naca-rm-l50g31
September 18, 1950

No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1950/naca-rm-l50g31.pdf