Abstract
A computer program for predicting the three-dimensional nonequilibrium viscous shock-layer flows over blunt sphere-cones at angle of attack has been developed. The method used is the viscous shock-layer approach for nonequilibrium, multicomponent ionizing air. Analysis of flowfields over a sphere-cone has been performed for both shock-slip and no-shock-slip conditions and the results are compared. This code is capable of analyzing equilibrium and noncatalytic wall boundary conditions, whereas the diffusion model is limited to binary diffusion. Results from this code have been compared with those from another code for the axisymmetric case, while the three-dimensional results are presented around the entire body at 10 deg angle of attack.
Published Version
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call