Parameter

4.7.3.11 prandtl plane

Prandtl Plane refers to a box wing aircraft configuration developed by Ludwig Prandtl based on his 1924 "Best Wing System" theory consisting of upper and lower wings connected by vertical surfaces forming a box-like structure providing minimum induced drag improved lift-to-drag ratio and increased passenger capacity with potential fuel savings and reduced emissions.

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