Book ChapterDOI
Development of Artificially Excited Disturbances in Supersonic Boundary Layer
Alexander D. Kosinov,A. A. Maslov +1 more
- pp 601-606
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TLDR
In this paper, a method of introducing the artificial regulable disturbances into supersonic boundary layer with the help of a point source of disturbances was suggested, and the experimental study of development of a spatial wave packet of a small intensity was carried out in the boundary layer of a flat plate.Abstract:
The present paper suggests a method of introducing the artificial regulable disturbances into supersonic boundary layer with the help of a point source of disturbances. While using the technique suggested the experimental study of development of a spatial wave packet of a small intensity was carried out in the boundary layer of a flat plate.read more
Citations
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Journal ArticleDOI
Experiments on the stability of supersonic laminar boundary layers
TL;DR: In this paper, an experimental study of the development of plane monochromatic waves in the boundary layer on a flat plate at Mach number M = 2.0 is presented.
Journal ArticleDOI
Numerical investigation of the nonlinear transition regime in a Mach 2 boundary layer
TL;DR: In this article, the authors investigated the transition process in a supersonic flat-plate boundary layer at Mach 2 using linear stability theory (LST) and direct numerical simulations (DNS).
Proceedings ArticleDOI
DNS of Complete Transition to Turbulence Via Oblique Breakdown at Mach 3: Part II
TL;DR: In this article, a set of six simulations was performed to study the development of a pair of oblique waves from their initiation at low amplitudes to the phase transition to turbulence.
Proceedings ArticleDOI
Investigation of Asymmetric Subharmonic Resonance in a Supersonic Boundary Layer at Mach 2 Using DNS
TL;DR: In this paper, the transition process in a supersonic at-plate boundary layer at Mach 2 is investigated numerically using linear stability theory (LST) and direct numerical simulations (DNS).
Proceedings ArticleDOI
Waves produced from a harmonic point source in a supersonic boundarylayer
P. Balakumar,M. Malik +1 more
References
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Journal ArticleDOI
Stability and transition of a supersonic laminar boundary layer on an insulated flat plate
John Laufer,Thomas Vrebalovich +1 more
TL;DR: In this article, self-excited oscillations have been discovered experimentally in a supersonic laminar boundary layer along a flat plate and the stability limits determined at free-stream Mach numbers 1·6 and 2·2.
Journal ArticleDOI
An experiment on the stability of hypersonic laminar boundary layers
TL;DR: In this paper, the hydrodynamic stability of the laminar hypersonic boundary layer was investigated with the aid of a hot-wire anemometer, and the demarcation boundaries for the amplification zone were found to resemble the corresponding limits of boundary-layer instability at lower speeds.
Related Papers (5)
Stability and transition of a supersonic laminar boundary layer on an insulated flat plate
John Laufer,Thomas Vrebalovich +1 more
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Y.H. Kuo,Donald Earl Ordway +1 more