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Wind-Tunnel Investigation at a Mach Number of 1.53 of an Airplane With a Triangular Wing
Author:
Scherrer, Richard
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A7J05
Link:
https://digital.library.unt.edu/ark:/67531/metadc58178/
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