NASA NTRS ยท 19720014686
Boundary condition computational procedures for inviscid, supersonic steady flow field calculations
Abstract
Results are given of a comparative study of numerical procedures for computing solid wall boundary points in supersonic inviscid flow calculatons. Twenty five different calculation procedures were tested on two sample problems: a simple expansion wave and a simple compression (two-dimensional steady flow). A simple calculation procedure was developed. The merits and shortcomings of the various procedures are discussed, along with complications for three-dimensional and time-dependent flows.
Keep this discovery
Explore connections, maps & timelines
Abbett, M. J.. 1971-11-30. Boundary condition computational procedures for inviscid, supersonic steady flow field calculations. https://ntrs.nasa.gov/citations/19720014686
Cite the original work for its findings. Save a collection to share your selection of sources.