Model for rocket-exhaust plumes calculates effects of heat, pressure, and particle-impingement on nearby structures. Model has potential industrial applications in studies of impingement of multiphase mixtures inside coalgasification equipment and turbines.
Exhaust-Plume Impingement Characteristics
NASA Tech Briefs ; 7 , 1
01.03.1983
Sonstige
Keine Angabe
Englisch
Numerical Study of Base Flow Induced by Exhaust Plume Impingement
British Library Conference Proceedings | 1998
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