Parameter

4.6.2.1.2 laminar nacelle

A laminar nacelle refers to an engine casing or housing designed to maintain laminar airflow over its surface, reducing drag and improving overall aircraft efficiency. Laminar flow is a type of airflow where air molecules move in parallel layers without turbulence, which can significantly reduce drag compared to turbulent flow. The design of a laminar nacelle typically involves smooth, curved surfaces, carefully shaped inlet and nozzle contours, and high-surface-quality manufacturing to minimize disturbances that could trigger turbulence. Often, laminar flow is maintained over 15–40% of the nacelle's surface, which can reduce aircraft drag by up to 1%.
By maintaining laminar flow, laminar nacelles contribute to reduced fuel consumption, lower emissions, and increased aircraft performance.

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
4.6.1 propulsor integration on airframe
4.6.2 converting shaft power to thrust
4.6.2.1 advanced nacelle
4.6.2.1.1 short nacelle
4.6.2.1.2 laminar nacelle
4.6.2.1.3 ducted fan
4.6.2.2 open rotor
4.6.2.3 rim-driven fan
4.6.2.4 tip-drive fan
4.6.2.5 variable pitch fan blades
4.6.2.6 multi-engine single propulsor
4.6.2.7 composite fan blades & containment
4.6.2.8 gas turbine technology
4.6.2.9 composite cycle engine
4.6.2.10 high speed electric propulsion
4.6.2.11 electric boosting of combustion engines
4.6.2.12 direct drive technology
4.6.2.13 gas turbine + fuel cell (sofc)
4.6.3 converting fuel to shaft power
4.6.4 non-combustion based engine integration
4.6.5 other propulsion technologies
4.7 aircraft structures

Scenario relevance

Number of parameter occurrence per scenario.

Input
Output
1
1
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