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Results:
1-7
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Results: 7
Authors:
Tang, KC
Brewster, MQ
Citation: Kc. Tang et Mq. Brewster, Nonlinear dynamic combustion in solid rockets: L effects, J PROPUL P, 17(4), 2001, pp. 909-918
Authors:
Hickman, SR
Brewster, MQ
Citation: Sr. Hickman et Mq. Brewster, Oscillatory combustion of Fine-AP/HTPB propellants: Disproportionate pyrolysis response, J PROPUL P, 16(5), 2000, pp. 867-873
Authors:
Brewster, MQ
Citation: Mq. Brewster, Solid propellant combustion response: Quasi-steady (QSHOD) theory development and validation, PROG ASTRON, 185, 2000, pp. 607-637
Authors:
Brewster, MQ
Ward, MJ
Son, SF
Citation: Mq. Brewster et al., Simplified combustion modeling of double base propellant: Gas phase chain reaction vs. thermal decomposition, COMB SCI T, 154, 2000, pp. 1-30
Authors:
Knott, GM
Brewster, MQ
Citation: Gm. Knott et Mq. Brewster, Two-dimensional combustion modeling of heterogeneous solid propellants with finite Peclet number, COMB FLAME, 121(1-2), 2000, pp. 91-106
Authors:
Tang, KC
Brewster, MQ
Citation: Kc. Tang et Mq. Brewster, Analysis of molecular gas radiation: Real gas property effects, J THERMOPHY, 13(4), 1999, pp. 460-466
Authors:
Louwers, J
Gadiot, GMHJL
Brewster, MQ
Son, SF
Parr, T
Hanson-Parr, D
Citation: J. Louwers et al., Steady-state hydrazinium nitroformate (HNF) combustion modeling, J PROPUL P, 15(6), 1999, pp. 772-777
Risultati:
1-7
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