NASA NTRS · 19800008769
Calculation of two-dimensional inlet flow fields in a supersonic free stream: Program documentation and test cases
Abstract
The use of a computer code for the calculation of two dimensional inlet flow fields in a supersonic free stream and a nonorthogonal mesh-generation code are illustrated by specific examples. Input, output, and program operation and use are given and explained for the case of supercritical inlet operation at a subdesign Mach number (M Mach free stream = 2.09) for an isentropic-compression, drooped-cowl inlet. Source listings of the computer codes are also provided.
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Biringen, S. H., Mcmillan, O. J.. 1980-03-01. Calculation of two-dimensional inlet flow fields in a supersonic free stream: Program documentation and test cases. https://ntrs.nasa.gov/citations/19800008769
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