Computational Methods for Inviscid Transonic Flows with Imbedded Shock Waves,
Abstract
A discussion is given of the methods for computing transonic flows with imbedded shock waves. Time dependent techniques, relaxation methods and approximate solutions are considered with emphasis placed on the latest developments. More details are given on the relaxation methods than other techniques. Computing times, accuracy, and proper treatment of shock waves are stressed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1971
- Accession Number
- AD0721933
Entities
People
- Earll M. Murman
Organizations
- Boeing