ADVANCED COMPRESSORS.
Abstract
Contents: Introductory remarks--recent progress in aerodynamic design of compressors; The through-flow analysis of axial flow compressors; Mass flow limitation in supersonic compressors; Transonic compressor cascades; Secondary flow losses in axial compressors; Basic elements for advanced designs of radial flow compressors; Supersonic radial diffusers; Supersonic cascade performance; Application of through flow to radial wheel design.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1970
- Accession Number
- AD0710893
Entities
Organizations
- AGARD