Conjugate Heat Transfer Simulation of a Subscale Rocket Thrust Chamber Using a Timescale Based Frozen Non-Adiabatic Flamelet Combustion Model

Titel:: Conjugate Heat Transfer Simulation of a Subscale Rocket Thrust Chamber Using a Timescale Based Frozen Non-Adiabatic Flamelet Combustion Model
Dokumenttyp:: Konferenzbeitrag
Autor(en):: Rahn, Daniel; Riedmann, Hendrik; Haidn, Oskar
Kongress- / Buchtitel:: AIAA Propulsion and Energy 2019 Forum
Verlag / Institution:: American Institute of Aeronautics and Astronautics
Publikationsdatum:: 16.08.2019
Jahr:: 2019
Volltext / DOI:: doi:10.2514/6.2019-3864
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