Parameter

4.1.2 krueger flap

Krueger flap leading-edge high-lift devices deflect downward to increase wing camber, significantly improving low-speed lift and aerodynamic performance during takeoff and landing. When integrated with advanced laminar flow wings, these devices help maintain a smooth boundary layer and prevent premature airflow separation. Challenges in developing these flaps include managing mechanical complexity and structural weight while ensuring seamless integration into thin composite leading edges.

Hierarchy

4 technological themes
4.1 active aircraft control
4.1.1 variable camber
4.1.2 krueger flap
4.1.3 blown flap
4.1.4 novel high-lift devices
4.1.5 active canards
4.1.6 airflow control (active)
4.1.7 adaptive wing
4.1.8 active load alleviation
4.1.9 variable cg management
4.1.10 full autonomous flight control
4.1.11 fast control loops for load control
4.1.12 active nacelle
4.1.13 variable geometry nacelle
4.1.14 fast actuation for gust load alleviation
4.1.15 optimized fuel 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

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