THE OPTIMUM INCIDENT ANGLE ON LOW-ASPECT-RATIO ROTOR BLADES OF A COMPRESSOR STAGE,
Abstract
Optimal incident angles in rotors with a blade aspect rate of 0.56 and solidity ratios of 1.15 and 1.77 were studied experimentally. A rotor with an aspect ratio of 0.84 and a solidity ratio of 1.18 was also tested.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 09, 1969
- Accession Number
- AD0700805
Entities
People
- V. V. Kovalevskii
Organizations
- National Air and Space Intelligence Center