Geodesic
Origins of turbulence on an unswept wing of supersonic transport
Matematičeskoe modelirovanie, Tome 34 (2022) no. 8, pp. 19-37 Cet article a éte moissonné depuis la source Math-Net.Ru

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The two most likely sources of disturbances capable of triggering boundary layer turbulization over the smooth unswept wing of supersonic transport are considered in the framework of full Navier-Stokes equations, namely: atmospheric turbulence and acoustic noise radiated by the turbulent boundary layer over the fuselage. Frequency wave characteristics of boundary layer disturbances over the wing are analyzed; the dominant mechanism of transition is revealed. Numerical results are compared with those of linear stability theory.
Keywords: supersonic transport, SST, unswept wing, origins of turbulence, atmospheric turbulence, numerical simulation, laminarization.
Mots-clés : acoustic noise 
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P. V. Chuvakhov; I. O. Pogorelov. Origins of turbulence on an unswept wing of supersonic transport. Matematičeskoe modelirovanie, Tome 34 (2022) no. 8, pp. 19-37. http://geodesic.mathdoc.fr/item/MM_2022_34_8_a1/

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