| 1 |
Ultra-Fine Aluminium Characterization and its Agglomeration Features in Solid Propellant Combustion for Various Quenched Distance and Pressure
Krishnarao T, Rao VV, Setty YP, Jayaraman K
Propellants Explosives Pyrotechnics, 45(5), 714, 2020 |
| 2 |
Analysis of aluminum particle combustion in a downward burning solid rocket propellant
Griego C, Yilmaz N, Atmanli A
Fuel, 237, 405, 2019 |
| 3 |
Sensitivity analysis and uncertainty quantification on aluminum particle combustion for an upward burning solid rocket propellant
Griego C, Yilmaz N, Atmanli A
Fuel, 237, 1177, 2019 |
| 4 |
Viscosity of rocket propellant (RP-1) at high temperatures and high pressures
Abdulagatov IM, Akhmedova-Azizova LA
Fuel, 235, 703, 2019 |
| 5 |
Measurements and modeling of the density of rocket propellant RP-2 at temperatures to 573 K and pressures to 100 MPa
Mallepally RR, Bamgbade BA, McHugh MA, Baled HO, Enick RM, Billingsley MC
Fuel, 253, 1193, 2019 |
| 6 |
Damage and Dilatometry for Solid Propellants with Digital Image Correlation
Miller TC
Propellants Explosives Pyrotechnics, 44(2), 234, 2019 |
| 7 |
Ignition delay time correlations for distillate fuels
Davidson DF, Zhu Y, Shao J, Hanson RK
Fuel, 187, 26, 2017 |
| 8 |
Experimental investigation of the factors affecting the burning rate of solid rocket propellants
Yaman H, Celik V, Degirmenci E
Fuel, 115, 794, 2014 |
| 9 |
Formulation of an RP-1 pyrolysis surrogate from shock tube measurements of fuel and ethylene time histories
MacDonald ME, Davidson DF, Hanson RK, Pitz WJ, Mehl M, Westbrook CK
Fuel, 103, 1051, 2013 |
| 10 |
Aging of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements
Cerri S, Bohn MA, Menke K, Galfetti L
Propellants Explosives Pyrotechnics, 38(2), 190, 2013 |
