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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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