NASA NTRS · 19810017541
Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects: Program documentation and test case
Abstract
The source listing of a computer code for calculating the flow fields in a supersonic free stream is given. The application of this code to an inlet on an airbreathing missile is also presented.
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Biringen, S., Mcmillan, O. J.. 1981-06-01. Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects: Program documentation and test case. https://ntrs.nasa.gov/citations/19810017541
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