NASA NTRS · 19690000146
Bell nozzle kernel analysis program
Abstract
Bell Nozzle Kernel Analysis Program computes and analyzes the supersonic flowfield in the kernel, or initial expansion region, of a bell or conical nozzle. It analyzes both plane and axisymmetric geometrices for specified gas properties, nozzle throat geometry and input line.
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Elliot, J. J., Stromstra, R. R.. 1969-05-01. Bell nozzle kernel analysis program. https://ntrs.nasa.gov/citations/19690000146
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