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The Coupling of a Preliminary Design Method with CFD Analysis for the Design of Heat Exchangers in Aviation

El-Soueidan, Mahmoud und Schmelcher, Marc und Häßy, Jannik und Görtz, Alexander (2024) The Coupling of a Preliminary Design Method with CFD Analysis for the Design of Heat Exchangers in Aviation. In: AIAA Aviation Forum and ASCEND, 2024. AIAA Aviation Forum and ASCEND 2024, 2024-07-29 - 2024-08-02, Las Vegas, Nevada, USA. doi: 10.2514/6.2024-4036. ISBN 978-162410716-0.

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Offizielle URL: https://arc.aiaa.org/doi/10.2514/6.2024-4036

Kurzfassung

A revolutionary and innovative propulsion concept has been presented by MTU Aero Engines: The Water-Enhanced Turbofan (WET). This concept implements a dual fluid thermodynamic cycle integrating heat exchangers into the core flow of the engine. An evaporator preheats, evaporates and superheats liquid water by cooling down the turbine exhaust flow. The generated steam is then injected into the core flow of the engine increasing efficiency and specific power of the engine. Heat Exchangers with phase change phenomena on at least one fluid side pose a novel component for aircraft engine industry. Therefore, suitable models in terms of low-fidelity tools are currently developed in order to assess the performance of such a novel component in a robust and numerically efficient way. At the DLR Institute of Propulsion Technology, a preliminary design tool for heat exchanger performance evaluation for aero engine applications is being developed (PreHEAT). A cell-based 0D P-NTU approach is applied to predict the thermodynamic performance of the heat exchanger setup. Literature correlations for both fluid sides are implemented determining the pressure loss and the transferred heat of the heat exchanger. The correlation-based prediction of the heat exchanger’s thermodynamic performance is accompanied by uncertainties. In order to reduce the uncertainty of the heat exchanger’s performance prediction using numerical methods, CFD results need to be fed back into the predesign tool. Therefore, in this paper, an approach is presented to couple the existing preliminary design tool with high-fidelity CFD results of the exhaust-side of the evaporator. The goal is to identify a suitable and numerically efficient method to feed back CFD results into PreHEAT and to integrate updated predesign results into the CFD simulation. The implemented coupling approach is finally demonstrated for a design point of the WET concept showing efficient and fast convergence of the coupled analysis.

elib-URL des Eintrags:https://elib.dlr.de/221278/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:The Coupling of a Preliminary Design Method with CFD Analysis for the Design of Heat Exchangers in Aviation
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
El-Soueidan, MahmoudMahmoud.El-Soueidan (at) dlr.dehttps://orcid.org/0009-0009-2614-8197199893555
Schmelcher, MarcMarc.Schmelcher (at) dlr.dehttps://orcid.org/0009-0009-7659-5358199893556
Häßy, JannikJannik.Haessy (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Görtz, AlexanderAlexander.Goertz (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:27 Juli 2024
Erschienen in:AIAA Aviation Forum and ASCEND, 2024
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Nein
DOI:10.2514/6.2024-4036
ISBN:978-162410716-0
Status:veröffentlicht
Stichwörter:Heat Exchangers, Computational Fluid Dynamics, Thermodynamic Cycles
Veranstaltungstitel:AIAA Aviation Forum and ASCEND 2024
Veranstaltungsort:Las Vegas, Nevada, USA
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:29 Juli 2024
Veranstaltungsende:2 August 2024
Veranstalter :American Institute of Aeronautics and Astronautics - AIAA
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Umweltschonender Antrieb
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L CP - Umweltschonender Antrieb
DLR - Teilgebiet (Projekt, Vorhaben):L - Triebwerkskonzepte und -integration
Standort: Köln-Porz
Institute & Einrichtungen:Institut für Antriebstechnik > Triebwerk
Hinterlegt von: El-Soueidan, Mahmoud
Hinterlegt am:16 Dez 2025 13:40
Letzte Änderung:16 Dez 2025 13:40

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