Abstract

For the efficient use of vector computers, three problems in the area of computational aerodynamics are dealt with. These are: 3-D full potential equation, body-fitted grid generation for wing-body configurations and 3-D Euler equations. Special features of each of these problems are emphasized. Various techniques to overcome the bottlenecks appearing therein are described.

Full Text
Published version (Free)

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