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

Author: Christensen, Frederik B.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A53L22
Link: https://digital.library.unt.edu/ark:/67531/metadc59957/

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