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Wind-Tunnel Investigation at Transonic Speeds of a Jet Control on a 35 Degree Swept Wing: Transonic-Bump Method
Author:
Vogler, Raymond D.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55K09
Link:
https://digital.library.unt.edu/ark:/67531/metadc61814/
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