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Visualization of the Detonation Wave Structure in a Small-Scale Hydrogen–Oxygen Rotating Detonation Combustor

Armbruster, Wolfgang und Bard, Ewen und Börner, Michael und Rheindorf, Kilian und Martin, Jan und Lober, Leon und General, Stephan und Hardi, Justin (2026) Visualization of the Detonation Wave Structure in a Small-Scale Hydrogen–Oxygen Rotating Detonation Combustor. Aerospace, 13. Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/aerospace13020158. ISSN 2226-4310.

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Kurzfassung

This study presents the high-speed visualization of the detonation wave structure in a smallscale hydrogen–oxygen rotating detonation combustor. A 68 mm Rotating Detonation Combustor was modified with a quartz-glass ring, such that radial optical access into the annular detonation chamber was realized. The optical access window covers approximately the first 22 mm of the detonation chamber. The modified experiment was hot-fire tested with the propellant combination gaseous hydrogen–oxygen. Simultaneous high-speed imaging from the back-end of the chamber and normal to the chamber axis allows a thorough investigation of the detonation wave characteristics. Both high-speed cameras were operated at 180,000 frames per second in order to resolve and capture the detonation waves. The downstream camera was used in order to investigate the number of waves and the spinning direction. A stable regime of three co-rotating waves was observed. The wave speed achieved 71% of the theoretical CJ-velocity. The second camera recorded the passing detonation waves through a quartz ring via OH* emissions. From the post-processed OH* images, a better understanding of the detonation wave structure, including the filling height of the fresh gas mixture as well as the approximate angles of the detonation and the shock wave, could be gained. The obtained height of the detonation wave is about 11–12 mm or 6–7 detonation cell sizes for the given setup and experimental conditions.

elib-URL des Eintrags:https://elib.dlr.de/222720/
Dokumentart:Zeitschriftenbeitrag
Titel:Visualization of the Detonation Wave Structure in a Small-Scale Hydrogen–Oxygen Rotating Detonation Combustor
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Armbruster, WolfgangWolfgang.Armbruster (at) dlr.dehttps://orcid.org/0000-0002-4859-4173205354366
Bard, EwenONERA, DMPE, Multi-physics department for energy, Palaiseau, FranceNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Börner, MichaelMichael.Boerner (at) dlr.dehttps://orcid.org/0000-0002-3441-2869205354367
Rheindorf, Kiliankilian.rheindorf (at) dlr.dehttps://orcid.org/0009-0002-6643-7662205354368
Martin, JanJan.Martin (at) dlr.dehttps://orcid.org/0000-0002-5050-2506205354369
Lober, Leonleon.lober (at) dlr.dehttps://orcid.org/0009-0007-7272-2351205354370
General, Stephanstephan.general (at) dlr.dehttps://orcid.org/0000-0001-5606-882XNICHT SPEZIFIZIERT
Hardi, JustinJustin.Hardi (at) dlr.dehttps://orcid.org/0000-0003-3258-5261NICHT SPEZIFIZIERT
Datum:7 Februar 2026
Erschienen in:Aerospace
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Ja
In SCOPUS:Ja
In ISI Web of Science:Ja
Band:13
DOI:10.3390/aerospace13020158
Verlag:Multidisciplinary Digital Publishing Institute (MDPI)
ISSN:2226-4310
Status:veröffentlicht
Stichwörter:rotating detonation engine; pressure gain combustion; hydrogen–oxygen; detonation wave structure; rocket engine
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - DRASTIC | Detonationsverbrennung für RaumfahrtAntriebsSysTeme: intensive Charakterisierung
Standort: Lampoldshausen
Institute & Einrichtungen:Institut für Raumfahrtantriebe > Raketenantriebstechnologie
Hinterlegt von: Armbruster, Wolfgang
Hinterlegt am:11 Feb 2026 08:06
Letzte Änderung:11 Feb 2026 08:06

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