NASA NTRS · 19660011753
Application of Lax's finite-difference method to nonequilibrium hypersonic flow problems
Abstract
Finite difference method for unsteady flows applied to steady state equations for supersonic region of inviscid flow past two-dimensional and axisymmetric bodies
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
De Jarnette, F. R.. 1966-03-01. Application of Lax's finite-difference method to nonequilibrium hypersonic flow problems. https://ntrs.nasa.gov/citations/19660011753
Cite the original work for its findings. Save a collection to share your selection of sources.