Design and Evaluation of a High Temperature Radial Turbine.
Abstract
Detailed performance predictions are presented. The second and third nozzle castings were received for evaluation, and the first bicast rotor for destructive spin-test was delivered. The replacement test rotor was machined, balanced, spin-tested, and used in the assembly of Turbine Build One. The rig was mounted on the test stand and cold flow testing was completed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 18, 1970
- Accession Number
- AD0866590
Entities
People
- G. S. Calvert
Organizations
- Pratt & Whitney