Simulation of dynamic fracture events in solid propellant rockets

Philippe H Geubelle, Changyu Hwang, Robert Fiedler, M. Scot Breitenfeld, Andreas Haselbacher

Research output: Contribution to conferencePaper

Abstract

This paper summarizes the formulation, implementation and preliminary application of an axisymmetric aeroelastic coupling algorithm specially developed to simulate the complex phenomena associated with dynamic fracture events taking place along the case/grain interface during the flight of a solid propellant rocket. The coupling approach combines an explicit cohesive/volumetric finite element (CVFE) scheme used to model the spontaneous initiation and rapid propagation of the interfacial crack, with an unstructured adaptive finite volume fluid solver able to capture the geometrical changes taking place in the fluid domain due to the crack motion and the large grain deformations. An Arbitrary Lagrangian/Eulerian (ALE) formulation is also adopted for the solid solver to account for the regressing boundary of the solid propellant. Nonlinear kinematics is used to describe the motion of the grain to account for the possible large deformations and rotations associated with the dynamic fracture process. The constitutive response of the grain is characterized by the Arruda-Boyce nonlinear model. Two applications illustrating the capabilities of the aeroeiastic code are presented in this paper: the first one is concerned with the motion of an inhibitor protruding in the core flow, and the second with the Titan IV SRMU grain collapse incident.

Original languageEnglish (US)
StatePublished - Dec 1 2001
Event37th Joint Propulsion Conference and Exhibit 2001 - Salt Lake City, UT, United States
Duration: Jul 8 2001Jul 11 2001

Other

Other37th Joint Propulsion Conference and Exhibit 2001
CountryUnited States
CitySalt Lake City, UT
Period7/8/017/11/01

Fingerprint

Solid propellants
Rockets
Cracks
Fluids
Kinematics

ASJC Scopus subject areas

  • Energy Engineering and Power Technology
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

Cite this

Geubelle, P. H., Hwang, C., Fiedler, R., Scot Breitenfeld, M., & Haselbacher, A. (2001). Simulation of dynamic fracture events in solid propellant rockets. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States.

Simulation of dynamic fracture events in solid propellant rockets. / Geubelle, Philippe H; Hwang, Changyu; Fiedler, Robert; Scot Breitenfeld, M.; Haselbacher, Andreas.

2001. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States.

Research output: Contribution to conferencePaper

Geubelle, PH, Hwang, C, Fiedler, R, Scot Breitenfeld, M & Haselbacher, A 2001, 'Simulation of dynamic fracture events in solid propellant rockets' Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States, 7/8/01 - 7/11/01, .
Geubelle PH, Hwang C, Fiedler R, Scot Breitenfeld M, Haselbacher A. Simulation of dynamic fracture events in solid propellant rockets. 2001. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States.
Geubelle, Philippe H ; Hwang, Changyu ; Fiedler, Robert ; Scot Breitenfeld, M. ; Haselbacher, Andreas. / Simulation of dynamic fracture events in solid propellant rockets. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States.
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