University of Illinois Urbana-Champaign

Multi-scale modeling of solid rocket motors: Time integration methods from computational aerodynamics applied to stable quasi-steady motor burning

Stewart, D. Scott; Tang, Kung-Chyun; Yoo, Sunhee; Brewster, M. Quinn; Kuznetsov, Igor R.

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https://hdl.handle.net/2142/312

Description

Title
Multi-scale modeling of solid rocket motors: Time integration methods from computational aerodynamics applied to stable quasi-steady motor burning
Author(s)
  • Stewart, D. Scott
  • Tang, Kung-Chyun
  • Yoo, Sunhee
  • Brewster, M. Quinn
  • Kuznetsov, Igor R.
Issue Date
2004-10
Abstract
Here we consider the problem of efficiently computing the stable burn-back of a solid rocket motor when the motor is in the quasi-steady burning regime of operation. When the motor is modeled as a cavity that is filled with a compressible fluid with normal mass and momentum and energy injection from the solid propellant surface, the problem posed is a standard one in steady computational aerodynamics.
Publisher
Department of Theoretical and Applied Mechanics (UIUC)
Series/Report Name or Number
TAM Reports 1054, (2004)
ISSN
0073-5264
Type of Resource
text
Language
en
Permalink
http://hdl.handle.net/2142/312

Owning Collections

Technical Reports - Theoretical and Applied Mechanics (TAM) PRIMARY
TAM technical reports include manuscripts intended for publication, theses judged to have general interest, notes prepared for short courses, symposia compiled from outstanding undergraduate projects, and reports prepared for research-sponsoring agencies.