Search NASA⌕ Search

NASA NTRS · 19860003783

Shuttle vertical fin flowfield by the direct simulation Monte Carlo method

Abstract

The flow properties in a model flowfield, simulating the shuttle vertical fin, determined using the Direct Simulation Monte Carlo method. The case analyzed corresponds to an orbit height of 225 km with the freestream velocity vector orthogonal to the fin surface. Contour plots of the flowfield distributions of density, temperature, velocity and flow angle are presented. The results also include mean molecular collision frequency (which reaches 1/60 sec near the surface), collision frequency density (approaches 7 x 10 to the 18/cu m sec at the surface) and the mean free path (19 m at the surface).

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Hueser, J. E., Brock, F. J., Melfi, L. T.. 1985-09-01. Shuttle vertical fin flowfield by the direct simulation Monte Carlo method. https://ntrs.nasa.gov/citations/19860003783

Cite the original work for its findings. Save a collection to share your selection of sources.