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Solution of inverse problem of the theory of nonsteady solid propellant combustion under the pressure drop in rocket engine

Novozhilov, B, Marshakov, V and Novozhilov, Vassili (2018) Solution of inverse problem of the theory of nonsteady solid propellant combustion under the pressure drop in rocket engine. In: ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, 3rd July 2018 - 6th July 2018, Yerevan, Armenia.

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Item Type: Conference or Workshop Item (Paper)
ISBN: 9780735417724
Uncontrolled Keywords: propellant; combustion; nozzle expansion ratio; thermal diffusivity
Subjects: FOR Classification > 0913 Mechanical Engineering
Faculty/School/Research Centre/Department > Centre for Environmental Safety and Risk Engineering (CESARE)
SWORD Depositor: Symplectic Elements
Depositing User: Symplectic Elements
Date Deposited: 27 Jun 2019 06:02
Last Modified: 27 Jun 2019 06:02
URI: http://vuir.vu.edu.au/id/eprint/38777
DOI: https://doi.org/10.1063/1.5081588
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Citations in Scopus: 0 - View on Scopus

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