An edge-based solution-adaptive method applied to the AIRPLANE code

An edition of An edge-based solution-adaptive method applied to the AIRPLANE code (1995)

An edge-based solution-adaptive method applied to the AIRPLANE code

By Rupak Biswas

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1995

Publisher

Research Institute for Advanced Computer Science, NASA Ames Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Pressure distribution, Transonic flow, Near fields, Unstructured grids (Mathematics), Flow distribution, Aircraft configurations, Sonic booms, Grid generation (Mathematics), Supersonic flow, Shock waves