Optimum fan pressure ratio for bypass engines with separate or mixed exhaust streams | Semantic Scholar
Parametric Study of a Turbojet Engine With Auxiliary Bypass Combustion- The TurboAux Engine
Aerospace | Free Full-Text | Assessment of a Turbo-Electric Aircraft Configuration with Aft-Propulsion Using Boundary Layer Ingestion
Turbofan Thrust
Fan Pressure Ratio Vs Thrust Vs TIT | Download Scientific Diagram
Turbofan - Wikipedia
The fan of a turbofan engine has a flow rate of 125.0 kg/s and The fan of a undergoes a pressure ratio of 1.5 to 1. The isentropic fn efficiency, \eta_{c} is
Fan Pressure - an overview | ScienceDirect Topics
Thermodynamic and Aerodynamic Analysis of an Air-Driven Fan System in Low-Cost High-Bypass-Ratio Turbofan Engine
Parametric Study of Turbofan Performance - ppt download
GE analysis post Farnborough - Leeham News and Analysis
Fan pressure ratio as function of reduced mass flow for the studied... | Download Scientific Diagram
Jet engine - Turbofan, Bypass Ratio, and Thrust Reversal | Britannica
GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO - diagram, schematic, and image 01
Performance map of a modern civil fan showing pressure ratio and... | Download Scientific Diagram
Fan Pressure - an overview | ScienceDirect Topics
Fan Basics: Air Flow, Static Pressure, and Impedance