NASA NTRS · 19850000382
Analysis of Scramjet Inlets
Abstract
NASCRIN analyzes two-dimensional flow fields in supersonic combustion ramjet (scramjet) inlets. Solves two-dimensional Euler or Navier-Strokes equations in conservative form by unsplit, explicit, two-step finitedifference method. More recent explicit/implicit, two-step scheme also incorporated for viscous flow analysis. Algebraic, two-layer eddy-viscosity model used for turbulent flow calculations.
Keep this discovery
Explore connections, maps & timelines
Kumar, A.. 1986-01-01. Analysis of Scramjet Inlets. https://ntrs.nasa.gov/citations/19850000382
Cite the original work for its findings. Save a collection to share your selection of sources.