검색결과 : 8건
No. | Article |
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1 |
Study of Maximum Pressure Rise with Erosive Burning in Multi-Grain Tubular Solid Propellant Ropia B, Upadhyay J, Kalal R, Shekhar H, Thakur DG Propellants Explosives Pyrotechnics, 45(9), 1398, 2020 |
2 |
Study of Maximum Pressure Rise with Erosive Burning in Multi-Grain Tubular Solid Propellant Ropia B, Upadhyay J, Kalal R, Shekhar H, Thakur DG Propellants Explosives Pyrotechnics, 45(9), 1398, 2020 |
3 |
Combustion characteristics of solid propellants under high-temperature dense-particle erosion conditions Li J, Ma K, Lv X, Liu PJ, He GQ, Liu Y, Chen J Combustion and Flame, 204, 49, 2019 |
4 |
Study on Dynamic Burning Rate Equation of Propellant Zhang RH, Rui XT, Wang Y, Li C Propellants Explosives Pyrotechnics, 42(6), 683, 2017 |
5 |
A model for erosive burning of homogeneous propellants Zhang J, Jackson TL Combustion and Flame, 157(2), 397, 2010 |
6 |
Spatial linear analysis of the flow in a solid rocket motor with burning walls Massa L Combustion and Flame, 156(4), 865, 2009 |
7 |
The effects of turbulence-induced time-periodic shear on a flame anchored to a propellant Isfahani AHG, Zhang J, Jackson TL Combustion and Flame, 156(5), 1084, 2009 |
8 |
A MODEL OF AP/HTPB COMPOSITE PROPELLANT COMBUSTION IN ROCKET-MOTOR ENVIRONMENTS Cai WD, Thakre P, Yang V Combustion Science and Technology, 180(12), 2143, 2008 |