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Conjugate heat and mass transfer at heterogeneous burning surface of AP/HTPB/Al composite propellant at 2–10 MPa

  • Published:2023-06 Issue: Volume:227 Page:120362
  • ISSN:1359-4311
  • Container-title:Applied Thermal Engineering
  • language:en
  • Short-container-title:Applied Thermal Engineering

Author:

Liu Shuyuan,Han Luyang,He Pengxiang,Wang Limin,Han Jinchao,Hu Songqi

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology,Fluid Flow and Transfer Processes,Mechanical Engineering

Reference32 articles.

1. Comprehensive view of the combustion models of composite solid propellants;Kishore;AIAA,1979

2. Model for steady state combustion of unimodal composite solid propellants;King;AIAA,1978

3. Performance of AP-based composite propellant containing nanoscale aluminum;Stephens;J. Propul. Power,2010

4. J.C. Thomas, G.R. Morrow, et al., Comprehensive study of AP particle size and loading effects on the burning rates of composite AP/HTPB propellants, in: 54th AIAA Joint Propulsion Conference, 2018.

5. Effect of crystal morphology of ammonium perchlorate on the properties of HTPB propellant;Zhu;Chinese J. Energetic Mater.,2016

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