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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.
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.
Issue Date:2004-10
Publisher:Department of Theoretical and Applied Mechanics (UIUC)
Series/Report:TAM Reports 1054, (2004)
Genre:Technical Report
Publication Status:published or submitted for publication
Peer Reviewed:is peer reviewed
Date Available in IDEALS:2007-03-09
Is Version Of:Published as: D Scott Stewart, K C Tang, Sunhee Yoo, Quinn Brewster, Igor R Kuznetsov. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV; USA; January 10-13. 2005. pp. 6789-6798 (10). Copyright 2005 American Institute of Aeronautics and Astronautics Inc.

This item appears in the following Collection(s)

  • Technical Reports - Theoretical and Applied Mechanics (TAM)
    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.

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