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The effects on the aerodynamic characteristics of varying the wing thickness ratio of a triangular wing-body configuration at transonic speeds from tests by the NACA wing-flow method
Author:
Hall, Albert W.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52B18
Link:
https://digital.library.unt.edu/ark:/67531/metadc59166/
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