Rotor Blade of a Turbomachine,
Abstract
The report describes various geometric configurations suggested for the root of a turbine blade in order to alleviate stress nonuniformity.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1973
- Accession Number
- AD0762219
Entities
People
- G. I. Bogoradovskii
Organizations
- National Air and Space Intelligence Center