Comparison of the Drag of a Fin-Stabilized Body of Revolution and of a Complete Airplane Configuration as Obtained at Transonic Speeds in a Slotted Wind Tunnel and in Free Flight

Author: Howell, Robert R.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L55H09
Link: https://digital.library.unt.edu/ark:/67531/metadc64268/

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