Parallel multiscale simulation of hypersonic flow with porous wall injection
Attributed to:
Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.4203/ccp.112.11
Publication URI: http://dx.doi.org/10.4203/ccp.112.11
Type: Conference/Paper/Proceeding/Abstract