elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Accessibility | Contact | Deutsch
Fontsize: [-] Text [+]

Highly Aggressive Inter Compressor Duct With Active Flow Control Part 2: Numerical Validation of Pulsed Jet Actuators With Unsteady Simulations

Fritz, Stefan and Koppers, Felix and Hergt, Alexander and Bresemann, David and Eck, Mario and Peitsch, Dieter and Möller, Felix and Rückert, Roland (2025) Highly Aggressive Inter Compressor Duct With Active Flow Control Part 2: Numerical Validation of Pulsed Jet Actuators With Unsteady Simulations. In: 70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition, GT 2025, pp. 1-13. 70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition, 2025-06-16 - 2025-06-20, Memphis, Tennessee, USA. doi: 10.1115/GT2025-152898. ISBN 978-079188887-2.

Full text not available from this repository.

Official URL: https://asmedigitalcollection.asme.org/GT/proceedings-abstract/GT2025/88872/V011T33A003/1220784

Abstract

The application of active flow control (AFC) methods in an inter compressor duct (ICD) offers the possibility of further length reduction while suppressing separations. In particular, pulsed jet actuators (PJAs) are advantageous because the pulsation enhances mixing processes. However, the PJAs require fluid that has already been compressed by the downstream high pressure compressor. Therefore, injecting this high momentum fluid from a downstream component makes this approach very expensive. Consequently, a highly optimized design is required to achieve the maximum separation suppression while minimizing the external energy. However, the numerical optimization requires steady simulations to find an optimum design in manageable time scales. Therefore, this study helps understanding if any aspects of unsteadiness are neglected by optimizing the PJA implementation with steady methods. Furthermore, the influence of the steady state assumption in the optimization is quantified. The influence of the unsteadiness of the PJA is investigated by comparing steady and unsteady simulations. The unsteady simulations include unsteady Reynolds-averaged Navier-Stokes and delayed detached-eddy simulation. The numerical simulations are validated against experimental data, obtained at the TU Berlin ICD test rig. After evaluating the different approaches, a conclusion is drawn on how unsteady flow control methods can be efficiently optimized. Consequently, the study shows that all the methods investigated have their advantages and disadvantages. Their use must be carefully selected according to the objective of the investigation.

Item URL in elib:https://elib.dlr.de/214910/
Document Type:Conference or Workshop Item (Speech)
Additional Information:Die Veröffentlichung ist im Rahmen des Projektes RDuct im LuFo Förderprogramm (LuFo VI-2, Fördernummer 20Q2110) des Bundesministerium für Wirtschaft und Energie entstanden.
Title:Highly Aggressive Inter Compressor Duct With Active Flow Control Part 2: Numerical Validation of Pulsed Jet Actuators With Unsteady Simulations
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Fritz, StefanUNSPECIFIEDhttps://orcid.org/0009-0002-7371-4269195277270
Koppers, FelixUNSPECIFIEDhttps://orcid.org/0009-0004-6613-9627195277271
Hergt, AlexanderUNSPECIFIEDhttps://orcid.org/0009-0008-1643-7326195277272
Bresemann, DavidILR, TU BerlinUNSPECIFIEDUNSPECIFIED
Eck, MarioUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Peitsch, DieterTechnical University of BerlinUNSPECIFIEDUNSPECIFIED
Möller, FelixUNSPECIFIEDhttps://orcid.org/0000-0002-0192-3873195277273
Rückert, RolandNAVASTO GmbHUNSPECIFIEDUNSPECIFIED
Date:11 August 2025
Journal or Publication Title:70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition, GT 2025
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.1115/GT2025-152898
Page Range:pp. 1-13
ISBN:978-079188887-2
Status:Published
Keywords:unsteady simulations, inter compressor duct, active flow control
Event Title:70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition
Event Location:Memphis, Tennessee, USA
Event Type:international Conference
Event Start Date:16 June 2025
Event End Date:20 June 2025
Organizer:The American Society of Mechanical Engineers
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Components and Emissions
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Institute of Test and Simulation for Gas Turbines > Virtual Engine and Numerical Methods
Deposited By: Fritz, Stefan
Deposited On:27 Oct 2025 11:38
Last Modified:27 Oct 2025 11:38

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
OpenAIRE Validator logo electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.