NASA NTRS · 19740000236
Numerical program for analysis of three-dimensional supersonic exhaust flow fields (CHAR 3D)
Abstract
Choice of reference plane orientation depends on specific nozzle geometry, with different configurations requiring different reference plane systems. In addition, for given configuration several reference systems may be used in different regions of flow field, so each system is locally aligned with flow.
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Dash, S., Guidice, P. D., Ferri, A., Roffe, G.. 1974-12-01. Numerical program for analysis of three-dimensional supersonic exhaust flow fields (CHAR 3D). https://ntrs.nasa.gov/citations/19740000236
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