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Some preliminary results in the determination of aerodynamic derivatives of control surfaces in the transonic speed range by means of a flush-type electrical pressure cell
Author:
Erickson, Albert L.
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A8H03
Link:
https://digital.library.unt.edu/ark:/67531/metadc57948/
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