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
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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