NASA NTRS · 19720000070
Design of two-dimensional sharp-edged-throat supersonic nozzle with boundary-layer correction
Abstract
Computer program accounts for effective nozzle geometry changes due to boundary layer displacement thickness. Program input and output are discussed.
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Goldman, L. J., Vanco, M. R.. 1972-01-01. Design of two-dimensional sharp-edged-throat supersonic nozzle with boundary-layer correction. https://ntrs.nasa.gov/citations/19720000070
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