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Multiphase Science and Technology

Erscheint 4 Ausgaben pro Jahr

ISSN Druckformat: 0276-1459

ISSN Online: 1943-6181

SJR: 0.144 SNIP: 0.256 CiteScore™:: 1.1 H-Index: 24

Indexed in

NUMERICAL BENCHMARK TEST NO. 1.2: MONOPROPELLANT ROCKET

Volumen 3, Ausgabe 1-4, 1987, pp. 459-461
DOI: 10.1615/MultScienTechn.v3.i1-4.260
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ABSTRAKT

The test problem considered is that of the injection of monopropellant droplets through small holes in one end of a rocket motor, which burn at a rate dependent upon the droplet diameter. The task is to compute the distance from the injector at which the propellant is fully consumed, as functions of the injection velocity, the propellant and combustion-product properties and relative speed. A two-fluid model is to be used with allowance for mass transfer between phases.

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