Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Lateral Control and Directional Stability and Control Characteristics of Model Equipped With Drooped, Supersonic-Type, Elliptical Wing-Root Inlet

Author: Cancro, Patrick A.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SL55J10
Link: https://digital.library.unt.edu/ark:/67531/metadc53255/

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