NASA NTRS · 19690054791
Heat transfer and thermal boundary layer in a conical nozzle.
Abstract
Inlet thermal boundary layer thickness effect on conical nozzle heat transfer and boundary layer determined by operating nozzle with cooled/ uncooled inlet
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Boldman, D. R., Graham, R. W.. 1969-06-01. Heat transfer and thermal boundary layer in a conical nozzle.. https://ntrs.nasa.gov/citations/19690054791
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