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Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location

Ralph P Bielat, P. K. Pierpont

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Abstract

Aerodynamic characteristics of aircraft configuration for low level supersonic attack tested in transonic wind tunnel

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Aerodynamic characteristics of aircraft configuration for low level supersonic attack tested in transonic wind tunnel

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Available abstract

Aerodynamic characteristics of aircraft configuration for low level supersonic attack tested in transonic wind tunnel

Key concepts: Airplane, Wing, Transonic, Aerodynamics, Wing configuration, Swept wing, Wing loading, Variable (mathematics)

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Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location — Research Paper | ScholarLens