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      Numerical investigation on regression rate and thrust regulation behaviors of a combined solid rocket motor with aluminum-based fuel

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      Aerospace Science and Technology
      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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              Flame propagation in weightlessness above the burning surface of material

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                Author and article information

                Journal
                Aerospace Science and Technology
                Aerospace Science and Technology
                Elsevier BV
                12709638
                December 2021
                December 2021
                : 119
                : 107102
                Article
                10.1016/j.ast.2021.107102
                11d879cd-1b07-4dfd-a545-2f3775792039
                © 2021

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

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