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Experimental and numerical investigation of spray characteristics in a new FLOX® based combustor for liquid fuels for Micro Gas Turbine Range Extender (MGT-REX)

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Publication date
1 January 2016
Publisher
'American Institute of Aeronautics and Astronautics (AIAA)'
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      oaiinfo:doi/10.2514%2F6.2016-4698
      Last time updated on 03/08/2021

      Institute of Transport Research:Publications

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      oaioai:elib.dlr.de:106283
      Last time updated on 19/02/2017