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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