Parameter

4.7.3.4 riblets

Riblets are small longitudinal grooves or ridges (about 0.1 mm wide) on an aircraft's surface, inspired by shark skin, designed to reduce drag by manipulating the boundary layer flow. Riblets work by disrupting turbulent streamwise vortices near the surface, reducing momentum exchange and thereby reducing skin friction drag (which accounts for >40% of total aircraft drag). They are typically used on wings, fuselages, and other areas where drag reduction is critical. Riblets can achieve 4–8% viscous drag reduction, resulting in improved fuel efficiency (up to 2% overall aircraft drag reduction when applied to entire airframe) and reduced CO₂ emissions. They can be applied as adhesive-backed film that can be retrofitted to existing aircraft

Hierarchy

4 technological themes
4.1 active aircraft control
4.2 data transfer technologies
4.3 energy carriers
4.4 net zero technologies
4.5 operational technologies
4.6 aircraft propulsion
4.7 aircraft structures
4.7.1 aerospace materials & manufacturing
4.7.2 aircraft fuselage
4.7.3 aircraft wings
4.7.3.1 in-wing energy storage
4.7.3.2 morphing structures
4.7.3.3 wing smart structures
4.7.3.4 riblets
4.7.3.5 flow control (passive) on wings
4.7.3.6 high aspect ratio wing
4.7.3.7 foldable winglets
4.7.3.8 foldable wings
4.7.3.9 flexible skin
4.7.3.10 laminar wings
4.7.3.11 prandtl plane
4.7.3.12 truss-braced wing
4.7.3.13 tube and wing optimization
4.7.3.14 wing bio-mimicry
4.7.3.15 passive load alleviation
4.7.3.16 wing structure as conductor
4.7.3.17 light/low mass paint/decals on wings
4.7.3.18 passive canards
4.7.3.19 in-flight cleaning of natural laminar flow leading edges
4.7.4 secondary structures

Scenario relevance

Number of parameter occurrence per scenario.

Input
Output
1
2
Optimising together
N/A
Stripping down
N/A
Tech for you
N/A
Mad max

Milestone Timehorizon

PESTEL categories

Current

Short term

Medium term

Long term

Little to many relations with other Milestones