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Effect of Full-Span Trailing-Edge Elevons on the Transonic Longitudinal Aerodynamic Characteristics of a Wing-Body Combination Having a 3-Percent-Thick Triangular Wing With 60 Degree Leading-Edge Sweep

Chris C Critzos, W. E. Foss

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Abstract

Report presenting the results of an investigation to determine the effects of full-span trailing-edge flaps on the static longitudinal characteristics of a triangular wing-body combination. Data was obtained for the basic configuration and for a wing with the control surfaces deflected for longitudinal control.

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What this paper is about

Report presenting the results of an investigation to determine the effects of full-span trailing-edge flaps on the static longitudinal characteristics of a triangular wing-body combination. Data was obtained for the basic configuration and for a wing with the control surfaces deflected for longitudinal control.

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Available abstract

Report presenting the results of an investigation to determine the effects of full-span trailing-edge flaps on the static longitudinal characteristics of a triangular wing-body combination. Data was obtained for the basic configuration and for a wing with the control surfaces deflected for longitudinal control.

Key concepts: Wing, Trailing edge, Wing configuration, Aerodynamics, Transonic, Leading edge, Wing loading, Span (engineering)

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Effect of Full-Span Trailing-Edge Elevons on the Transonic Longitudinal Aerodynamic Characteristics of a Wing-Body Combination Having a 3-Percent-Thick Triangular Wing With 60 Degree Leading-Edge Sweep — Research Paper | ScholarLens