Investigation on unsteady thermal process of NEPE propellant based on an refined chemical kinetic model

Author:

Chen Kaixuan,Ye Zhenwei,Yu Yizhe,Xue XiaochunORCID,Yu Yonggang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference45 articles.

1. Miller M.S., and W.R. Anderson. "Energetic-material combustion modeling with elementary gas-phase reactions - a practical approach." 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): 501-531. Brewster, M. Q. solid Propellant Combustion Response: Quasi-Steady (QSHOD) Theory Development and validation. AIAA J., 2(16) (2000) 607–637.

2. A model of composite solid propellant combustion based on multiple flames;Beckstead;AIAA J.,1970

3. Numerical analysis of AP/HTPB composite propellant combustion under rapid depressurization;Cao;Appl. Therm. Eng.,2015

4. Numerical simulation of quenched combustion model for AP/HTPB propellant under transient depressurization;Ye;Propellants Explos. Pyrotech.,2017

5. Unsteady chemical kinetics behavior of AP/HTPB propellant with micro-scale model;Xue;Combust. Sci. Technol.,2018

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