COMPARISONS OF PREDICTIONS WITH NUMERICAL BENCHMARK TEST NO. 1.2: MONOPROPELLANT ROCKET

Dudley Brian Spalding; K. Taylor

doi:10.1615/MultScienTechn.v6.i1-4.270

Multiphase Science and Technology

Главный редактор: Akio Tomiyama (open in a new tab)

Редактор-основательs: Jean-Marc Delhaye (open in a new tab) Geoffrey F. Hewitt (open in a new tab) Novak Zuber (open in a new tab)

Ассоциированный редакторs: Gioia Falcone (open in a new tab) Arun Kumar Nayak (open in a new tab) Masahiro Kawaji (open in a new tab) Shu Takagi (open in a new tab)

Выходит 4 номеров в год

ISSN Печать: 0276-1459

ISSN Онлайн: 1943-6181

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COMPARISONS OF PREDICTIONS WITH NUMERICAL BENCHMARK TEST NO. 1.2: MONOPROPELLANT ROCKET

Том 6, Выпуск 1-4, 1992, pp. 547-554

DOI: 10.1615/MultScienTechn.v6.i1-4.270

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Dudley Brian Spalding
Concentration, Heat, and Momentum (CHAM), Limited, Bakery House, 40 High Street, Wimbledon Village, London SW19 5AU, England

K. Taylor
Concentration, Heat and Momentum Ltd.(CHAM), Bukey House, 40 High Street, Wimbledon Village, London, SW11 5AU, England

Краткое описание

Predictions using the PHOENICS and MINCS codes were compared with Numerical Benchmark Test No. 1.1 for a monopropellant rocket (D. B. Spalding, Multiphase Science and Technology, Vol. 3, pp.459−461, 1987). The agreement between the numerical calculations and the exact solution is quite good for both codes, although there are minor discrepancies in predicted phase volume fraction and drop diameter.

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