Aviation & Aircraft Icing Research

In modern aviation, icing is no longer only a safety problem—it is a performance and efficiency challenge.

Even small changes in surface condition, flow behavior, or ice formation can significantly impact aerodynamic efficiency, system performance, and operational cost.

We support research and development efforts aimed at understanding and optimizing these effects at a fundamental level.

From Safety to Efficiency

While icing has traditionally been addressed from a safety perspective, today’s aircraft development focuses increasingly on efficiency.

Key drivers include:

  • Reduction of fuel consumption
  • Shift toward electrification and the elimination of bleed air for heating.
  • Optimization of aerodynamic performance
  • Minimization of operational costs
  • Improvement of system reliability

In this context, even very small performance changes—on the order of fractions of a percent—can translate into significant economic impact over an aircraft’s lifetime.

The Importance of Surface Condition & Laminarity

Modern aircraft designs increasingly rely on laminar flow to achieve high aerodynamic efficiency.

However, laminar flow is highly sensitive to surface disturbances.

Icing-related effects such as:

  • Small-scale roughness
  • Localized ice accretion
  • Runback water and re-freezing

can trigger premature transition to turbulent flow, leading to:

  • Increased drag
  • Reduced efficiency
  • Higher fuel consumption

Understanding and controlling these effects is a key challenge in current aircraft development.

Advanced Icing Phenomena

Beyond classical icing scenarios, several complex phenomena are of increasing importance:

Runback Water & Secondary Icing

Water that is not immediately frozen can flow along the surface and re-freeze in downstream regions.

This leads to:

  • Ice formation outside protected areas
  • Complex and difficult-to-predict accretion patterns
  • Strong influence on aerodynamic performance

Runback icing is a major challenge in modern ice protection system design.

Ice Crystal Icing

Ice crystal icing occurs at high altitudes and is particularly relevant for:

  • Engine components
  • Sensors and probes
  • Internal flow systems

Unlike classical icing, ice crystals can:

  • Bounce, fragment, or partially melt on impact
  • Accumulate in complex ways
  • Lead to unexpected blockage or performance degradation
  • Damage to from detached ice chunks

Understanding these mechanisms requires detailed experimental investigation.

Interaction of Systems & Surfaces

Modern aircraft systems are highly integrated.

Key interactions include:

Optimizing one aspect can negatively affect another, making system-level understanding essential.

Experimental Support for Simulation & Modeling

Advanced aircraft development increasingly relies on simulation tools.

However, these tools require high-quality experimental data for:

  • Model validation
  • Calibration of physical models
  • Development of new simulation approaches

We support:

This enables more accurate and reliable simulation results.

Component-Level Research

We focus on component-level investigations that are critical for system performance:

These studies provide detailed insight into physical processes and their impact on overall system behavior.

Supporting Innovation in Aviation

Our work supports:

This includes both application-driven development and research-oriented projects.

Who This Is For

This page is particularly relevant for:

  • Aircraft manufacturers and OEMs
  • Tier suppliers and system developers
  • Research organizations and simulation developers
  • Companies working on advanced aerodynamic concepts

Frequently Asked Questions

Yes. While safety aspects are well understood, performance and efficiency impacts remain a major area of research.

Laminar flow depends on extremely smooth surface conditions. Even small disturbances such as roughness or thin ice layers can trigger transition to turbulence.

Yes, high-quality experimental data is essential for validating and improving simulation models.

No, these effects are relevant across different aircraft types, especially where efficiency is critical.