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Results:
1-10
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Results: 10
Authors:
Xu, CH
Bunnell, RA
Heister, SD
Citation: Ch. Xu et al., On the influence of internal flow structure on performance of plain-orifice atomizers, AT SPRAYS, 11(4), 2001, pp. 335-349
Authors:
Yoon, SS
Heister, SD
Epperson, JT
Sojka, PE
Citation: Ss. Yoon et al., Modeling multi-jet mode electrostatic atomization using boundary element methods, J ELECTROST, 50(2), 2001, pp. 91-108
Authors:
Yoon, SS
Heister, SD
Citation: Ss. Yoon et Sd. Heister, Analytic solution for fluxes at interior points for the 2D Laplace equation, ENG ANAL, 24(2), 2000, pp. 155-160
Authors:
Wernimont, EJ
Heister, SD
Citation: Ej. Wernimont et Sd. Heister, Combustion experiments in hydrogen peroxide/polyethylene hybrid rocket with catalytic ignition, J PROPUL P, 16(2), 2000, pp. 318-326
Authors:
Bunnell, RA
Heister, SD
Citation: Ra. Bunnell et Sd. Heister, Three-dimensional unsteady simulation of cavitating flows in injector passages, J FLUID ENG, 122(4), 2000, pp. 791-797
Authors:
Schoonover, PL
Crossley, WA
Heister, SD
Citation: Pl. Schoonover et al., Application of a genetic algorithm to the optimization of hybrid rockets, J SPAC ROCK, 37(5), 2000, pp. 622-629
Authors:
Bunnell, RA
Heister, SD
Yen, C
Collicott, SH
Citation: Ra. Bunnell et al., Cavitating injector flows: Validation of numerical models and simulations of pressure atomizers, AT SPRAYS, 9(5), 1999, pp. 445-465
Authors:
Moses, MP
Collicott, SH
Heister, SD
Citation: Mp. Moses et al., Detection of aerodynamic effects in liquid jet breakup and droplet formation, AT SPRAYS, 9(4), 1999, pp. 331-342
Authors:
Wernimont, EJ
Heister, SD
Citation: Ej. Wernimont et Sd. Heister, Reconstruction technique for reducing hybrid-rocket combustion test data, J PROPUL P, 15(1), 1999, pp. 128-136
Authors:
Murray, IF
Heister, SD
Citation: If. Murray et Sd. Heister, On a droplet's response to acoustic excitation, INT J MULT, 25(3), 1999, pp. 531-550
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