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Thermostructural Numerical Analysis of the Thrust Chamber of a Liquid Propellant Rocket Engine

Roberto Citarella1, Michele Ferraiuolo2, Michele Perrella3

  • 1Department of Industrial Engineering, University of Salerno, 84084 Fisciano, SA, Italy.

Materials (Basel, Switzerland)
|August 12, 2022
PubMed

Keywords:
creepfinite element methodliquid rocket enginelow-cycle fatigueplasticitystress analysisthermal stress

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