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Performance and economic assessment of a wing-integrated hybrid laminar flow control system

Fröhler, Benjamin and Pohya, Ahmad Ali and Häßy, Jannik and Kilian, Thomas and Bismark, Alexander Heinz and Radestock, Martin and Cruz Palacios, David (2025) Performance and economic assessment of a wing-integrated hybrid laminar flow control system. The Aeronautical Journal, pp. 1-28. Cambridge University Press. doi: 10.1017/aer.2025.26. ISSN 0001-9240.

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Official URL: https://www.cambridge.org/core/journals/aeronautical-journal/article/performance-and-economic-assessment-of-a-wingintegrated-hybrid-laminar-flow-control-system/040885D53933FFB5DDF6B0B2F4EC140E

Abstract

The energy efficiency of emerging aircraft designs plays a key role, not only in reducing environmental impact, but also in reducing operating costs in the anticipated rise in fuel prices. The European Clean Sky 2 project HLFC-Win is investigating the feasibility of hybrid laminar flow control (HLFC) technology integrated into the outer wing leading edge for a long-haul aircraft. HLFC technology reduces aerodynamic friction drag by means of suction of the boundary layer through a micro-perforated skin to achieve laminarity and thereby improving aircraft performance. However, integrating such a system is not without its drawbacks, as the integration has an impact on the geometry, mass, aerodynamics and engine offtakes that need to be considered. Therefore, the aim of this current work is to assess the HLFC system based on a fair, objective and transparent comparison between the HLFC aircraft and an aircraft of the same technology level without HLFC. The assessment of the HLFC system is twofold, firstly estimating the mission-based performance at the overall aircraft level and secondly performing a lifecycle simulation with three scenarios to determine realistic fuel and cost savings. The mission-based performance assessment indicates a block fuel reduction of over 3 % for the design mission which averages 1.6 to 2.5 % considering a realistic route scenario and expected degradation. The economic assessment suggests a dependency on the scenario chosen, ranging from a 0.7 % increase in total cost (in an unfavourable scenario) to almost a 1 % reduction in total cost (in a favourable scenario), equivalent to $15 million saved per HLFC aircraft over its lifetime. These results support the commercial viability of HLFC technology, which offers significant aerodynamic and fuel efficiency improvements and operating cost savings to the aviation industry. Importantly, no critical barriers were identified for the integration of HLFC technology, further underscoring its potential to improve aircraft performance.

Item URL in elib:https://elib.dlr.de/213771/
Document Type:Article
Title:Performance and economic assessment of a wing-integrated hybrid laminar flow control system
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Fröhler, BenjaminUNSPECIFIEDhttps://orcid.org/0000-0001-5695-1671183309916
Pohya, Ahmad AliUNSPECIFIEDhttps://orcid.org/0000-0002-2734-3199UNSPECIFIED
Häßy, JannikUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Kilian, ThomasUNSPECIFIEDhttps://orcid.org/0000-0003-1395-608XUNSPECIFIED
Bismark, Alexander HeinzUNSPECIFIEDhttps://orcid.org/0000-0001-8150-9877183309918
Radestock, MartinUNSPECIFIEDhttps://orcid.org/0000-0002-9918-3315183309920
Cruz Palacios, DavidUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:April 2025
Journal or Publication Title:The Aeronautical Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.1017/aer.2025.26
Page Range:pp. 1-28
Publisher:Cambridge University Press
ISSN:0001-9240
Status:Published
Keywords:hybrid laminar flow control; overall aircraft design; life cycle simulation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Aircraft and  Validation
Location: Braunschweig , Hamburg , Köln-Porz
Institutes and Institutions:Institute of Maintenance, Repair and Overhaul
Institute of Propulsion Technology
Institute of Flight Systems
Institut für Systemleichtbau
Institut für Systemleichtbau > Adaptronics
Institute of System Architectures in Aeronautics > Aviation System Concepts and Assessment
Institute of Propulsion Technology > Engine
Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Fröhler, Benjamin
Deposited On:22 Apr 2025 17:54
Last Modified:08 Jan 2026 11:53

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