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An Investigation of Four Wings of Square Plan Form at a Mach Number of 6.86 in the Langley 11-Inch Hypersonic Tunnel
Author:
McLellan, Charles H.
Additional Authors:
Bertram, Mitchel H.
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51D17
Link:
https://digital.library.unt.edu/ark:/67531/metadc58952/
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