Parameter

4.7.3.13 tube and wing optimization

Tube and wing optimization refers to the design process of optimizing the shape and structure of an aircraft's fuselage (tube) and wings to minimize drag maximize lift and improve overall aerodynamic efficiency while also considering factors such as structural integrity weight and manufacturability.

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
3
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