Abstract
Contamination of the aircraft leading edges by insects and other airborne particles is a major operational concern for the implementation of hybrid laminar flow control (HLFC) - an active drag reduction technique, which has the potential to produce significant fuel savings for airliners. A review of the critical issues is provided, encompassing the transition mechanism, insect distributions and concepts for contamination mitigation. The use of liquid/foam-based systems has proved to be very successful, as is evident in the review of experimental work.
| Original language | English |
|---|---|
| Pages (from-to) | 267-277 |
| Number of pages | 11 |
| Journal | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering |
| Volume | 218 |
| Issue number | 4 |
| DOIs | |
| Publication status | Published - 2004 |
Keywords
- De-icing systems
- Insect contamination
- Laminar flow control (LFC)
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