Calculating Gas Flow in a Bypass Compressor,
Abstract
The report discusses a calculation scheme for finding a number of solutions when designing a by-pass engine, where it is necessary to calculate also the flow in the compressor whose running section is divided into two annular channels by a longitudinal semibarrier extending downstream from a certain intermediate stage. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 23, 1973
- Accession Number
- AD0756092
Entities
People
- V. S. Salnilov
Organizations
- National Air and Space Intelligence Center