Turbofan Cycle, Performance and Design Analysis,
Abstract
A turbofan cycle analysis has been carried out to predict the effect of cycle independent variables - e.g. compressor pressure ratio, bypass ratio, fan pressure ratio and turbine entry temperature - on specific fuel consumption. Influence of these variables on engine performance for different flight conditions and engine ratings has been shown.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 20, 1975
- Accession Number
- ADA017798
Entities
People
- M. Simer
- T. Etlik
- Z. Masek
- Z. Pospisil
Organizations
- National Air and Space Intelligence Center