Publisher's Synopsis
A computational fluid dynamics tool has been developed capable of analyzing the viscous supersonic/hypersonic flow about realistic configurations. This techniques can predict the flow in regions of canopies, wings, and canards in addition to the usual simple symmetric configurations. It also allows for interactions between aerodynamic surfaces such as the vortex interaction between canards and wings. Chaussee, Denny S. Ames Research Center NASA-TM-100082, A-88118, NAS 1.15:100082 ...
