NASA NTRS · 19690054762
A theory for base pressures in multi-nozzle rocket configurations.
Abstract
Turbulent base flowfields in multinozzle configurations, considering adiabatic flow and determining base pressure distribution from reverse jet impingement
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Abbud, K. A., Lamb, J. P., Lenzo, C. S.. 1969-06-01. A theory for base pressures in multi-nozzle rocket configurations.. https://ntrs.nasa.gov/citations/19690054762
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