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      Mixing augmentation of transverse hydrogen jet by injection of micro air jets in supersonic crossflow

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      Acta Astronautica
      Elsevier BV

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          Hydrogen fuel rocket engines simulation using LOGOS code

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            Accumulation of errors in numerical simulations of chemically reacting gas dynamics

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              Characteristics of Dual Transverse Injection in Scramjet Combustor, Part 1: Mixing

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                Author and article information

                Journal
                Acta Astronautica
                Acta Astronautica
                Elsevier BV
                00945765
                August 2017
                August 2017
                : 137
                : 403-414
                Article
                10.1016/j.actaastro.2017.05.007
                dbbe21a5-cc64-4637-9449-cdc80b1d6735
                © 2017

                https://www.elsevier.com/tdm/userlicense/1.0/

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