TURBOMACHINE ROTOR BLADE,
Abstract
A turbomachine rotor blade with a shroud flange is described. To improve its rigidity without increasing its weight, the flange has a streamlined configuration.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 09, 1969
- Accession Number
- AD0693536
Entities
People
- A. G. Klebanov
Organizations
- National Air and Space Intelligence Center