The Low Hub-Tip Ratio Supersonic Axial-Flow Compressor. Volume IV.
Abstract
The report describes the overall and detail performance of the Mach 2 supersonic rotor at 70%, 84%, 90% and 100% of the design speed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1973
- Accession Number
- AD0773352
Entities
People
- Frans A. E. Breugelmans
Organizations
- von Kármán Institute for Fluid Dynamics