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- W1621104529 abstract "A numerical study of the response of aircraft wings to atmospheric gusts and to nuclear explosions when flying at subsonic speeds is presented. The method is based upon unsteady quasi-vortex lattice method, unsteady suction analogy and Pade approximant. The calculated results, showing vortex lag effect, yield reasonable agreement with experimental data for incremental lift on wings in gust penetration and due to nuclear blast waves." @default.
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- W1621104529 date "1983-04-01" @default.
- W1621104529 modified "2023-09-27" @default.
- W1621104529 title "Calculation of wing response to gusts and blast waves with vortex lift effect" @default.
- W1621104529 hasPublicationYear "1983" @default.
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