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    Experimental Investigation of Injection-Coupled High-Frequency Combustion Instabilities

    Freier Zugriff
    Armbruster, Wolfgang / Hardi, Justin S. / Oschwald, Michael | Springer Verlag | 2020

    Study of LOx/H2 Spray Flame Response to Acoustic Excitation in a Rectangular Rocket Combustor

    Hardi, Justin / Oschwald, Michael / Dally, Bassam B. | AIAA | 2013

    Acoustic characterisation of a rectangular rocket combustor with liquid oxygen and hydrogen propellants

    Hardi, Justin S / Oschwald, Michael / Dally, Bassam | SAGE Publications | 2013

    Numerical study of acoustic resonance in a LOX injector post induced by orifice flow

    Son, Min / Armbruster, Wolfgang / Tonti, Federica et al. | AIAA | 2021

    High-Speed Flame Radiation Imaging of Thermoacoustic Coupling in a High Pressure Research Thrust Chamber

    Armbruster, Wolfgang / Hardi, Justin / Suslov, Dimitry et al. | AIAA | 2018

    NUMERICAL STUDY OF ACOUSTIC RESONANCE IN A LOX INJECTOR POST INDUCED BY ORIFICE FLOW

    Son, Min / Armbruster, Wolfgang / Tonti, Federica et al. | TIBKAT | 2021

    Unsteady Modelling of LOx/GH2 Flame Response to Longitudinal Chamber Mode Forcing

    Tonti, Federica / Hardi, Justin / Karl, Sebastian et al. | AIAA | 2018

    Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines

    Armbruster, Wolfgang / Hardi, Justin S. / Miene, Yannik et al. | Elsevier | 2019

    Injector-Driven Flame Dynamics in a High-Pressure Multi-Element Oxygen–Hydrogen Rocket Thrust Chamber

    Armbruster, Wolfgang / Hardi, Justin S. / Suslov, Dmitry et al. | AIAA | 2019

    Coupling Behaviour of LOx/H2 Flames to Longitudinal and Transverse Acoustic Instabilities

    Hardi, Justin / Beinke, Scott / Oschwald, Michael et al. | AIAA | 2012

    Flame-acoustic interaction in a high-pressure, single-injector, LOX/CNG rocket combustor with optical access

    Martin, Jan / Armbruster, Wolfgang / Börner, Michael et al. | AIAA | 2023

    Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor

    Gröning, Stefan / Hardi, Justin S. / Suslov, Dmitry et al. | AIAA | 2016

    Flame-Acoustic Interaction in a High-Pressure, Single-Injector, LOX/CNG Rocket Combustor with Optical Access

    Martin, Jan / Armbruster, Wolfgang / Börner, Michael et al. | TIBKAT | 2023

    EXPERIMENTAL INVESTIGATION OF SELF-EXCITED COMBUSTION INSTABILITIES IN A LOX/LNG ROCKET COMBUSTOR

    Martin, Jan / Armbruster, Wolfgang / Hardi, Justin et al. | TIBKAT | 2020

    Experimental Investigation of Self-Excited Combustion Instabilities in a LOX/LNG Rocket Combustor

    Martin, Jan / Armbruster, Wolfgang / Hardi, Justin et al. | AIAA | 2020

    Experimental Investigation of Self-Excited Combustion Instabilities in a LOX/LNG Rocket Combustor

    Martin, Jan / Armbruster, Wolfgang / Hardi, Justin Steven et al. | AIAA | 2021

    Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines

    Armbruster, Wolfgang / Hardi, Justin S. / Miene, Yannik et al. | DataCite | 2020