An experimental investigation of four triangular-wing-body combinations in sideslip at Mach numbers 0.6, 0.9, 1.4, and 1.7

Christensen, Frederik B
naca-rm-a53l22
March 15, 1954


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-a53l22.pdf