Method of Calculating Dual-Rotor Compressors for Ducted-Fan Engines,
Abstract
Theoretical foundations for the choice of parameters and some practical suggestions for the calculation of a two-rotor axial compressor of a ducted-fan jet engine are given. A front-fan engine is considered. The method of optimum division of the mechanical energy between the inner and the outer air streams is presented. This method can be used for determining the basic parameters of the fan. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 27, 1968
- Accession Number
- AD0848387
Entities
People
- J. Traczyk
Organizations
- National Air and Space Intelligence Center