Ji et al., 2020 - Google Patents
Numerical analysis on combustion instabilities in end-burning-grain solid rocket motors utilizing pressure-coupled response functionsJi et al., 2020
- Document ID
- 5227986633165698511
- Author
- Ji S
- Wang B
- Zhao D
- Publication year
- Publication venue
- Aerospace Science and Technology
External Links
Snippet
The combustion instability has been one of severe problems suffered by solid rocket motors (SRMs) for a long term. This paper proposes a burning rate model utilizing the pressure- coupled response function for description of the spatiotemporal burning of AP-HTPB …
- 238000002485 combustion reaction 0 title abstract description 53
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