The aim of this paper is to analyze the aeroelastic processes developed during the starting phase of a rocket engine via a coupling fluid/structure code.
Solid rocket motor consists of a solid propellant grain embedded into a stronger metallic or composite case with an insulator material and a liner between the case and the grain.
Online Language Learning Tool SkELL allows users to search for phrases in sentences, collocates and similar words. These examples have been automatically selected and may contain errors.
