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Spanwise loading for wings and control surfaces of low aspect ratio

John Deyoung

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Abstract

From considerations of the linearized-compressible-flowequation, the aero@namic values given by zero-as~ct-ratio theory are also those of moderat=spect+atio wings at the speed applicable for low values of the product of pressibility parameter and aspect ratio.

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From considerations of the linearized-compressible-flowequation, the aero@namic values given by zero-as~ct-ratio theory are also those of moderat=spect+atio wings at the speed applicable for low values of the product of pressibility parameter and aspect ratio.

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Available abstract

From considerations of the linearized-compressible-flowequation, the aero@namic values given by zero-as~ct-ratio theory are also those of moderat=spect+atio wings at the speed applicable for low values of the product of pressibility parameter and aspect ratio.

Key concepts: Aspect ratio (aeronautics), Materials science, Composite material

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