NASA NTRS · 19750000018
Computer programs for calculating potential flow in propulsion system inlets
Abstract
Calculational procedure evolved in process of designing inlets. Douglas axisymmetric potential flow program called EOD calculates incompressible potential flow about arbitrary bodies. Program SCIRCL generates input for EOD from inlet components. Program COMBYN takes basic solutions output by EOD and combines them into solutions of interest and applied compressibility correction.
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Stockman, N. O., Button, S. L.. 1975-04-01. Computer programs for calculating potential flow in propulsion system inlets. https://ntrs.nasa.gov/citations/19750000018
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