Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack View Full Text


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Article Info

DATE

2018-08

AUTHORS

S. V. Lukashevich, S. O. Morozov, A. N. Shiplyuk

ABSTRACT

Experimental investigations are performed to understand the effect of the passive porous coating on the high-frequency disturbances and laminar–turbulent transition of a hypersonic boundary layer on the sharp cone with an apex half-angle Θc = 7° aligned at normalized angles of attack up to α = 1° at the Mach number M∞ = 5.8. It is demonstrated that the passive porous coating effectively suppresses the most unstable second-mode disturbances in the hypersonic boundary layer at the studied angles of attack. It is found that the passive porous coating delays the laminar–turbulent transition both on the windward and leeward sides. The reflection coefficient of the passive porous coating for ultrasonic acoustic waves is also measured. More... »

PAGES

130

References to SciGraph publications

  • 2016-09. Experimental study of the effect of a passive porous coating on disturbances in a hypersonic boundary layer 2. Effect of the porous coating location in JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS
  • 2013-08. An experimental study of the natural noise in the Transit-M hypersonic wind tunnel in THERMOPHYSICS AND AEROMECHANICS
  • 2010-12. Effect of the cone nose bluntness and the ultrasonically absorptive coating on transition in a hypersonic boundary layer in FLUID DYNAMICS
  • 2014-03. Boundary-layer stabilization by an ultrasonically absorptive material on a cone in hypersonic flow: numerical investigations in CEAS SPACE JOURNAL
  • 2012-12. Experimental study of the influence of parameters of a passive porous coating on the development of disturbances in a hypersonic boundary layer in TECHNICAL PHYSICS LETTERS
  • 2005-01. Theoritical analysis of acoustic instability of a hypersonic shock layer on a porous wall in JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS
  • 2014-06. Ultrasonic absorption characteristics of porous carbon–carbon ceramics with random microstructure for passive hypersonic boundary layer transition control in EXPERIMENTS IN FLUIDS
  • 2013-07. Experimental study of the effect of a passive porous coating on disturbances in a hypersonic boundary layer. 1. Effect of the porous coating length in JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS
  • 2015-02. The efficiency of the method of sound-absorbing coatings in vibrationally excited hypersonic flow in TECHNICAL PHYSICS LETTERS
  • 2005-01. Theoretical analysis of acoustic instability of a hypersonic shock layer on a porous wall in JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS
  • Identifiers

    URI

    http://scigraph.springernature.com/pub.10.1007/s00348-018-2585-1

    DOI

    http://dx.doi.org/10.1007/s00348-018-2585-1

    DIMENSIONS

    https://app.dimensions.ai/details/publication/pub.1105879940


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