Scale Effects on Solid Rocket Combustion Instability Behaviour

Article, Other literature type English OPEN
David R. Greatrix;
  • Publisher: Molecular Diversity Preservation International
  • Journal: Energies, volume 4, issue 1 1, pages 1-18 (issn: 1996-1073)
  • Publisher copyright policies & self-archiving
  • Identifiers: doi: 10.3390/en4010090
  • Subject: solid rocket motor | scale effects | combustion instability | Technology | combustion instability; solid rocket motor; scale effects | T
    • jel: jel:Q0 | jel:Q | jel:Q4 | jel:Q47 | jel:Q49 | jel:Q48 | jel:Q43 | jel:Q42 | jel:Q41 | jel:Q40

The ability to understand and predict the expected internal behaviour of a given solid-propellant rocket motor under transient conditions is important. Research towards predicting and quantifying undesirable transient axial combustion instability symptoms necessitates a... View more
  • References (13)
    13 references, page 1 of 2

    Blomshield, F.S. Historical Perspective of Combustion Instability in Motors: Case Studies. In Proceedings of AIAA/ASME/SAE/ASEE 37th Joint Propulsion Conference, Salt Lake City, UT, USA, 8-11 July 2001; AIAA Paper No. 2001-3875.

    Baum, J.D.; Levine, J.N.; Lovine, R.L. Pulsed instability in rocket motors: A comparison between predictions and experiments. J. Propul. Power 1988, 4, 308-316.

    3. Greatrix, D.R.; Harris, P.G. Structural Vibration Considerations for Solid Rocket Internal Ballistics Modeling. In Proceedings of AIAA/ASME/SAE/ASEE 36th Joint Propulsion Conference, Huntsville, AL, USA, 17-19 July 2000; AIAA Paper No. 2000-3804.

    4. Montesano, J.; Behdinan, K.; Greatrix, D.R.; Fawaz, Z. Internal chamber modeling of a solid rocket motor: Effects of coupled structural and acoustic oscillations on combustion. J. Sound Vib. 2008, 311, 20-28.

    5. Greatrix, D.R. Simulation of axial combustion instability development and suppression in solid rocket motors. Int. J. Spray Combust. Dyn. 2009, 1, 143-168.

    6. Greatrix, D.R. Transient burning rate model for solid rocket motor internal ballistic simulations. Int. J. Aerosp. Eng. 2008, 2008, 826070:1-826070:10.

    7. Greatrix, D.R. Model for prediction of negative and positive erosive burning. Can. Aeronaut. Space J. 2007, 53, 13-21.

    8. Greatrix, D.R. Inert particles for axial combustion instability suppression in a solid rocket motor. J. Propul. Power 2008, 24, 1347-1354.

    9. Gottlieb, J.J.; Greatrix, D.R. Numerical study of the effects of longitudinal acceleration on solid rocket motor internal ballistics. J. Fluids Eng. 1992, 114, 404-410.

    10. Baum, J.D.; Levine, J.N; Chew, J.S.B.; Lovine, R.L. Pulsed Instability in Rocket Motors: A Comparison between Predictions and Experiments. In Proceedings of 22nd AIAA Aerospace Sciences Meeting, Reno, NV, USA, 9-12 January 1984; AIAA Paper No. 84-0290.

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