NASA NTRS · 19870000129
Analysis of Scramjet Inlets
Abstract
NASCRIN program analyzes two-dimensional flow fields in supersoniccombustion ramjet (scramjet) inlets. Solves two-dimensional Euler or Navier-Stokes equations in conservative form by unsplit, explicit, two-step finite-difference method. More recent explicit/implicit, two-step scheme incorporated by analysis of viscous flow. Algebraic, two-layer eddy-viscosity model used for turbulent-flow calculations. Vectorized version, written for CDC CYBER 205, whereas scalar version, can be run on CRAY or other scalar computers.
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Kumar, A.. 1987-03-01. Analysis of Scramjet Inlets. https://ntrs.nasa.gov/citations/19870000129
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