Investigation of hybrid laminar flow control (HLFC) surfaces

T. M. Young, B. Humphreys, J. P. Fielding

Research output: Contribution to journalArticlepeer-review

Abstract

Hybrid laminar flow control (HLFC) is an active drag reduction technique. A delay in transition of the boundary layer from laminar to turbulent flow is usually achieved by the application of suction over the first 10-20% of the chord. The design of the suction surface and the chambers underneath the perforated skin represents one of the most significant engineering challenges concerning HLFC. A review of design requirements, candidate materials and drilling methods for the production of the suction surface, is presented. Materials considered include titanium, aluminium and carbon fibre composite. Laser (Excimer or Nd-YAG) and electron beam drilling has been used to produce satisfactory suction panels.

Original languageEnglish
Pages (from-to)127-146
Number of pages20
JournalAircraft Design
Volume4
Issue number2-3
DOIs
Publication statusPublished - Jun 2001

Keywords

  • Hybrid laminar flow control
  • Laser drilling
  • Suction surfaces

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