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
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Ji et al. | Numerical analysis on combustion instabilities in end-burning-grain solid rocket motors utilizing pressure-coupled response functions | |
| Karabeyoglu et al. | Modeling of hybrid rocket low frequency instabilities | |
| Ji et al. | Modeling and analysis of triggering pulse to thermoacoustic instability in an end-burning-grain model solid rocket motor | |
| Anand et al. | Investigation of pulse detonation combustors—Axial turbine system | |
| Kawane et al. | The influence of heat transfer and friction on the impulse of a detonation tube | |
| Su et al. | Improved method of measuring pressure coupled response for composite solid propellants | |
| Pieringer et al. | Simulation of combustion instabilities in liquid rocket engines with acoustic perturbation equations | |
| Fotia et al. | Experimental thrust sensitivity of a rotating detonation engine to various aerospike plug-nozzle configurations | |
| Razdan et al. | Erosive burning study of composite solid propellants by turbulent boundary-layer approach | |
| Haghdoost et al. | Mitigation of pressure fluctuations from an array of pulse detonation combustors | |
| Sardeshmukh et al. | High-pressure experiments relevant to rocket propulsion | |
| Mariappan et al. | Thermoacoustic instability in a solid rocket motor: non-normality and nonlinear instabilities | |
| Mawid et al. | Application of pulse detonation combustion to turbofan engines | |
| Habicht et al. | Acoustic modes in a plenum downstream of a multitube pulse detonation combustor | |
| Karabeyoglu et al. | Transient modeling of hybrid rocket low frequency instabilities | |
| Yang et al. | Bifurcation and nonlinear analysis of a time-delayed thermoacoustic system | |
| BUCKMASTER* | Pressure transients and the genesis of transverse shocks in unstable detonations | |
| Karthikeyan et al. | Quasi 1-D numerical analysis of combustion instability in hybrid rocket motor incorporating boundary layer lags | |
| Cuquel et al. | Prediction of the nonlinear dynamics of a multiple flame combustor by coupling the describing function methodology with a Helmholtz solver | |
| Nez et al. | Response of a transcritical coaxial flame to fuel injection rate modulations: Analysis and low-order modeling of the generation of unsteady heat release rate | |
| Fougnie et al. | Low order modeling of high frequency combustion instabilities in liquid rocket engines | |
| Priem | Theoretical and experimental models for unstable rocket combustor | |
| Jourdain et al. | Analysis of thermo-acoustic properties of combustors and afterburners | |
| Duchaine et al. | Sensitivity of flame transfer functions of laminar flames | |
| NUSCA | Numerical simulation of fluid dynamics with finite-rate and equilibrium combustion kinetics for the 120-mm ram accelerator |