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JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 2003 Volume 44, Issue 5, Pages 64–71 (Mi pmtf2538)

This article is cited in 19 papers

Nonlinear mechanisms of the initial stage of the laminar–turbulent transition at hypersonic velocities

A. N. Shiplyuka, D. A. Bountina, A. A. Maslova, N. Chokanib

a Lavrent'ev Institute of Hydrodynamics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
b State University of North Carolina, Rayleigh, 27695, USA

Abstract: Weakly nonlinear development of waves in an axisymmetric hypersonic boundary layer is studied by the method of bispectral analysis. The type of nonlinear interaction that was not observed previously in such flows is found. The possibility of subharmonic resonance of the second mode at the nonlinear stage of transition is demonstrated. The previously discovered nonlinear generation of the harmonic of the fundamental wave of the second mode of disturbances is observed.

Keywords: hypersonic, boundary layer, nonlinear interaction, bispectral analysis, bicoherence.

UDC: 532.526

Received: 31.03.2003


 English version:
Journal of Applied Mechanics and Technical Physics, 2003, 44:5, 654–659

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