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Numerical modelling of rocket combustors

Fechter, Stefan (2022) Numerical modelling of rocket combustors. DLR_Summer_School Lampoldshausen 2022, 2022-09-14, Lampoldshausen, Germany.

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Official URL: https://www.dlr.de/content/de/artikel/nachwuchs/dlr_summer_school_raumfahrtantriebe.html

Abstract

Introduction to the numerical simulation of cryogenic rocket combustion chambers and their numerical tools needed.

Item URL in elib:https://elib.dlr.de/192094/
Document Type:Conference or Workshop Item (Lecture)
Title:Numerical modelling of rocket combustors
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Fechter, StefanUNSPECIFIEDhttps://orcid.org/0000-0001-5683-4715UNSPECIFIED
Date:September 2022
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:numerical simulation, rocket combustion chamber
Event Title:DLR_Summer_School Lampoldshausen 2022
Event Location:Lampoldshausen, Germany
Event Type:Workshop
Event Date:14 September 2022
Organizer:DLR
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Project Amadeus
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Fechter, Stefan
Deposited On:15 Dec 2022 08:25
Last Modified:24 Apr 2024 20:53

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