1 |
Numerical Simulation and Unsteady Combustion Model of AP/HTPB Propellant under Depressurization by Rotation Ye ZW, Yu YG Propellants Explosives Pyrotechnics, 44(4), 493, 2019 |
2 |
Numerical Simulation of Quenched Combustion Model for AP/HTPB Propellant under Transient Depressurization Ye ZW, Yu YG Propellants Explosives Pyrotechnics, 42(9), 1085, 2017 |
3 |
DRIVING MECHANISMS FOR COMBUSTION INSTABILITY Sirignano WA Combustion Science and Technology, 187(1-2), 162, 2014 |
4 |
Study on Unsteady Combustion Behaviors of AP/HTPB Base-Bleed Propellants under Transient Depressurization Conditions Yu YG, Zhou YH, Lu CY, Xue XC Propellants Explosives Pyrotechnics, 39(4), 511, 2014 |
5 |
CO/NOX EMISSIONS OF STRONGLY PULSED JET DIFFUSION FLAMES Fregeau M, Hermanson JC Combustion Science and Technology, 181(3), 536, 2009 |
6 |
Bifurcations of propellant burning rate at oscillatory pressure Novozhilov BV Propellants Explosives Pyrotechnics, 31(3), 209, 2006 |
7 |
A model for the thermoacoustic response of a premixed swirl burner, -Part 1: Acoustic aspects Lawn CJ, Evesque S, Polifke W Combustion Science and Technology, 176(8), 1331, 2004 |
8 |
A model for the thermoacoustic response of a premixed swirl burner, -Part II: The flame response Lawn CJ, Polifke W Combustion Science and Technology, 176(8), 1359, 2004 |
9 |
Parametric studies of acoustic radiation from premixed flames Rajaram R, Lieuwen T Combustion Science and Technology, 175(12), 2269, 2003 |
10 |
Numerical simulation of self-excited combustion oscillations in a non-premixed burner Hantschk CC, Vortmeyer D Combustion Science and Technology, 174(1), 189, 2002 |