Test Cases for Numerical Methods in Two-Dimensional Transonic Flows,
Abstract
In order to provide test cases for the development of numerical methods for the computation of two-dimensional transonic flows round aerofoils, 6 aerofoil shapes have been selected for which accurate solutions are available. These include both symmetrical and cambered profiles, non-lifting and lifting, in subcritical and supercritical (shock-free) flow. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1970
- Accession Number
- AD0715554
Entities
People
- R. C. Lock
Organizations
- AGARD