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A Transonic Wind-Tunnel Investigation of the Performance and of the Static Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane, Ted No. NACA DE 390

Ralph P Bielat

Abstract

Report presenting an investigation of the aerodynamic characteristics of a model of the Grumman F9F-9 airplane in the transonic tunnel. Results regarding the transonic drag-rise increment, drag analysis, and effective downwash angle are provided.

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Available abstract

Key concepts: Downwash, Transonic, Airplane, Wind tunnel, Aerospace engineering, Drag, Aerodynamics, Subsonic and transonic wind tunnel