212
Views
0
CrossRef citations to date
0
Altmetric
Articles

Perturbation analysis of the Heterogeneous Quasi 1-D model – a theoretical framework for predicting frequency response of AP–HTPB composite solid propellants

&
Pages 852-871 | Received 28 Feb 2020, Accepted 10 May 2020, Published online: 28 May 2020

References

  • F.S. Blomshield, Historical perspective of combustion instability in motors: case studies, AIAA Paper 3875 (2001), p. 2001.
  • F. Blomshield, Lessons learned in solid rocket combustion instability, 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati, OH, 2007.
  • F. Vuillot and G. Casalis, Motor flow instabilities-part 1, Tech. Rep. RTO-EN-023, ONERA-MEUDON Centre, France, 2004.
  • Y.B. Zel'dovich, On theory of burning of the gunpowder and explosives, J. Exp. Theor. Phys. 12 (1942), pp. 498–524.
  • B.V. Novozhilov, Nonstationary combustion of solid rocket fuels, Tech. Rep. FTD-MT-24-317-74, DTIC Document, 1973.
  • F.E.C. Culick, A review of calculations for unsteady burning of a solid propellant, AIAA J. 6 (1968), pp. 2241–2255. doi: 10.2514/3.4980
  • M. Beckstead, A model for solid propellant combustion, Symposium (International) on Combustion, Vol. 18. Elsevier, 1981, pp. 175–185.
  • R.L. Glick, On statistical analysis of composite solid propellant combustion, AIAA J. 12 (1974), pp. 384–385. doi: 10.2514/3.49241
  • M. Shusser, F.E.C. Culick, and N.S. Cohen, Analytical solution for pressure-coupled combustion response functions of composite solid propellants, J. Propul. Power 24 (2008), pp. 1058–1067. doi: 10.2514/1.21502
  • J.A. Spurling, Modeling effects of initial temperatures on a propellant's pressure-coupled response using a pseudo propellant model, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, OH, 2014, p. 3494.
  • N.S. Cohen, Review of composite propellant burn rate modeling, AIAA J. 18 (1980), pp. 277–293. doi: 10.2514/3.50761
  • M.L. Gross and M.W. Beckstead, Diffusion flame calculations for composite propellants predicting particle-size effects, Combust. Flame 157 (2010), pp. 864–873. doi: 10.1016/j.combustflame.2009.09.004
  • T.L. Jackson and J. Buckmaster, Heterogeneous propellant combustion, AIAA J. 40 (2002), pp. 1122–1130. doi: 10.2514/2.1761
  • J. Buckmaster, T.L. Jackson, L. Massa, and M. Ulrich, Response of a burning heterogeneous propellant to small pressure disturbances, Proc. Combust. Inst. 30 (2005), pp. 2079–2086. doi: 10.1016/j.proci.2004.07.024
  • S. Varunkumar, M. Zaved, and H.S. Mukunda, A novel approach to composite propellant combustion modeling with a new heterogeneous quasi one-dimensional (HeQu1-D) framework, Combust. Flame 173 (2016), pp. 411–424. doi: 10.1016/j.combustflame.2016.07.031
  • M. Zaved, Steady heterogeneous quasi 1-D model for AP-HTPB based composite propellants, Master's thesis, Indian Institute of Technology, Madras, 2017. Available at https://home.iitm.ac.in/varuns/Thesis_Zaved_2017.pdf.
  • S. Varunkumar and H.S. Mukunda, Aluminized composite propellant combustion modeling with heterogeneous quasi-one dimensional (HeQu1-D) approach, Combust. Flame192 (2018), pp. 59–70. doi: 10.1016/j.combustflame.2018.01.042
  • F.S. Blomshield, C. Bicker, and R.A. Stalnaker, High pressure pulsed motor firing combustion instability investigations, 1997 AIAA Joint Propulsion Meeting, Paper, 97-3253, Seattle, WA, 1997.
  • V. Wadhai and S. Varunkumar, Linear instability and DC shift in tactical missile solid rocket motors – a computational study, 11th ASPACC, The University of Sydney, NSW Australia, 2017.
  • W. Vishal, Unsteady heterogeneous quasi 1D model for AP/HTPB based composite propellants, Master's thesis, Indian Institute of Technology, Madras, 2016. Available at https://home.iitm.ac.in/varuns/thesis_vishal.pdf.
  • T. Mitani and T. Niioka, Double flame structure in AP combustion, Symposium (International) on Combustion, Vol. 20. Elsevier, 1985, pp. 2043–2049.
  • G. Lengelle, J. Duterque, and J. Trubert, Physico-chemical mechanisms of solid propellant combustion, Solid propellant chemistry, combustion, and motor interior ballistics (A 00-36332 09-28), Reston, VA, American Institute of Aeronautics and Astronautics, Inc. (Progress in Astronautics and Aeronautics. 185 (2000), pp. 287–334.
  • R.R. Miller, Effects of particle size on reduced smoke propellant ballistics, AIAA paper, Cleveland, OH, 1982, p. 1096.
  • M. Ibiricu, Experimental studies on the oscillatory combustion of solid propellants, Rep. NWCTP4393, Naval Weapons Center, 1969.

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.