STRUCTURE OF THE FLOW IN RELATIVE MOTION AT THE INLET OF A CENTRIFUGAL COMPRESSOR IMPELLER.
Abstract
The results of investigating the three-dimensional flow at the inlet to the working vanes of a centrifugal compressor impeller are introduced with measurement of the parameters of flow in relative motion. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 19, 1966
- Accession Number
- AD0635832
Entities
People
- B. L. Gunbin
Organizations
- National Air and Space Intelligence Center