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MEMS Microphones for Wind Tunnel and Flight Tests

Ahlefeldt, Thomas and Ernst, Daniel and Carsten, Spehr (2026) MEMS Microphones for Wind Tunnel and Flight Tests. In: Numerical Methods and Experimental Means for the Integration of Future Propulsion Systems Springer Aerospace Technology, 1. Springer Cham. pp. 185-201. doi: 10.1007/978-3-031-97725-1_10. ISBN 978-3-031-97724-4. ISSN 1869-1730.

Full text not available from this repository.

Official URL: https://link.springer.com/book/10.1007/978-3-031-97725-1_10

Abstract

The application of micro-electro-mechanical systems (MEMS) microphones in the field of aeroacoustics has gained significant attention in recent years. Traditional measurement techniques often struggle with size, weight, and cost limitations, making MEMS microphones an attractive alternative. Nevertheless, the utilization of MEMS microphones for aeroacoustic measurements reveals some challenges to overcome regarding the field of application (i.e. aircraft, wind tunnel), the data acquisition, the calibration and typical implementation problems in general. The following article will briefly summarize the preparation and calibration of MEMS sensors for inflight aeroacoustic measurements as well as two flight testing campaigns performed on DLR aircraft.

Item URL in elib:https://elib.dlr.de/224617/
Document Type:Book Section
Additional Information:https://link.springer.com/book/10.1007/978-3-031-97725-1
Title:MEMS Microphones for Wind Tunnel and Flight Tests
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Ahlefeldt, Thomasthomas.ahlefeldt (at) dlr.dehttps://orcid.org/0000-0002-2869-2665UNSPECIFIED
Ernst, Danieldaniel.ernst (at) dlr.dehttps://orcid.org/0000-0001-7920-9162215880499
Carsten, Spehrcarsten.spehr (at) dlr.dehttps://orcid.org/0000-0002-2744-3675215880500
Date:2 May 2026
Journal or Publication Title:Numerical Methods and Experimental Means for the Integration of Future Propulsion Systems
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:1
DOI:10.1007/978-3-031-97725-1_10
Page Range:pp. 185-201
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Boden, Fritzfritz.boden (at) dlr.dehttps://orcid.org/0000-0001-9653-3802215880501
Publisher:Springer Cham
Series Name:Springer Aerospace Technology
ISSN:1869-1730
ISBN:978-3-031-97724-4
Status:Published
Keywords:Microphone array, Turbulent boundary layer,Kapton foil,Flight test,Wave number decomposition,Propeller noise,Spatial resolution,Flexible circuit board
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: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Experimental Methods, GO
Deposited By: Micknaus, Ilka
Deposited On:27 May 2026 11:45
Last Modified:03 Jun 2026 08:16

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