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

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

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

Kurzfassung

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.

elib-URL des Eintrags:https://elib.dlr.de/213771/
Dokumentart:Zeitschriftenbeitrag
Titel:Performance and economic assessment of a wing-integrated hybrid laminar flow control system
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Fröhler, BenjaminBenjamin.Froehler (at) dlr.dehttps://orcid.org/0000-0001-5695-1671183309916
Pohya, Ahmad AliAhmad.Pohya (at) dlr.dehttps://orcid.org/0000-0002-2734-3199NICHT SPEZIFIZIERT
Häßy, JannikJannik.Haessy (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Kilian, ThomasThomas.Kilian (at) dlr.dehttps://orcid.org/0000-0003-1395-608XNICHT SPEZIFIZIERT
Bismark, Alexander HeinzAlexander.Bismark (at) dlr.dehttps://orcid.org/0000-0001-8150-9877183309918
Radestock, MartinMartin.Radestock (at) dlr.dehttps://orcid.org/0000-0002-9918-3315183309920
Cruz Palacios, DavidNICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:April 2025
Erschienen in:The Aeronautical Journal
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
DOI:10.1017/aer.2025.26
Seitenbereich:Seiten 1-28
Verlag:Cambridge University Press
ISSN:0001-9240
Status:veröffentlicht
Stichwörter:hybrid laminar flow control; overall aircraft design; life cycle simulation
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Effizientes Luftfahrzeug
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L EV - Effizientes Luftfahrzeug
DLR - Teilgebiet (Projekt, Vorhaben):L - Virtuelles Flugzeug und Validierung
Standort: Braunschweig , Hamburg , Köln-Porz
Institute & Einrichtungen:Institut für Systemarchitekturen in der Luftfahrt
Institut für Instandhaltung und Modifikation
Institut für Antriebstechnik
Institut für Aerodynamik und Strömungstechnik
Institut für Flugsystemtechnik
Institut für Systemleichtbau
Institut für Systemleichtbau > Adaptronik
Hinterlegt von: Fröhler, Benjamin
Hinterlegt am:22 Apr 2025 17:54
Letzte Änderung:02 Mai 2025 12:09

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