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Bypass ratio

  • Aerospace Engine Data

    Aerospace Engine Data

  • 2. Afterburners

    2. Afterburners

  • Clean Sky 2 JU Work Plan 2014/2015

    Clean Sky 2 JU Work Plan 2014/2015

  • An Investigation Into the Feasibility of Using a Dual-Combustion Mode Ramjet in a High Mach Number Tactical Missile

    An Investigation Into the Feasibility of Using a Dual-Combustion Mode Ramjet in a High Mach Number Tactical Missile

  • Design of a Turbofan Engine Cycle with Afterburner for a Conceptual UAV

    Design of a Turbofan Engine Cycle with Afterburner for a Conceptual UAV

  • 04 Propulsion

    04 Propulsion

  • An Online Performance Calculator for Ramjet, Turbojet, Turbofan, and Turboprop Engines

    An Online Performance Calculator for Ramjet, Turbojet, Turbofan, and Turboprop Engines

  • Characteristics of the Specific Fuel Consumption for Jet Engines

    Characteristics of the Specific Fuel Consumption for Jet Engines

  • Design and Control of a Variable Geometry Turbofan with an Independently Modulated Third Stream

    Design and Control of a Variable Geometry Turbofan with an Independently Modulated Third Stream

  • TF-CLAWS: Candidate Low-Bypass, Mixed-Flow Turbofan Engine for a Next Generation Trainer

    TF-CLAWS: Candidate Low-Bypass, Mixed-Flow Turbofan Engine for a Next Generation Trainer

  • A Parametric Analysis of a Turbofan Engine with an Auxiliary Bypass Combustion Chamber – the Turboaux Engine

    A Parametric Analysis of a Turbofan Engine with an Auxiliary Bypass Combustion Chamber – the Turboaux Engine

  • Airbus Technical Magazine April 2020

    Airbus Technical Magazine April 2020

  • Airplane Flying Handbook (FAA-H-8083-3B) Chapter 15

    Airplane Flying Handbook (FAA-H-8083-3B) Chapter 15

  • THE TURBOFAN ENGINE the Turbofan Engine Is a Propulsive Mechanism to Combine the High Thrust of a Turbojet with the High Efficiency of a Propeller

    THE TURBOFAN ENGINE the Turbofan Engine Is a Propulsive Mechanism to Combine the High Thrust of a Turbojet with the High Efficiency of a Propeller

  • Parametric Study of a Turbojet Engine with Auxiliary Bypass Combustion- the Turboaux Engine

    Parametric Study of a Turbojet Engine with Auxiliary Bypass Combustion- the Turboaux Engine

  • An Overview of Propulsion Systems for Flying Vehicles

    An Overview of Propulsion Systems for Flying Vehicles

  • Study of Bypass Ratio Increasing Possibility for Turbofan Engine and Turbofan with Inter Turbine Burner

    Study of Bypass Ratio Increasing Possibility for Turbofan Engine and Turbofan with Inter Turbine Burner

  • Turbofan Engine Bypass Ratio As a Function of Thrust and Fuel Flow

    Turbofan Engine Bypass Ratio As a Function of Thrust and Fuel Flow

Top View
  • Innovative Double Bypass Engine for Increased Performance
  • Conceptual Development of Quiet Turbofan Engines for Supersonic Aircraft
  • Advanced Propulsion System Studies in High Speed Research
  • Appendix: Engine Data Tables
  • Passport Cf34-10
  • Aerothermodynamic Cycle Analysis of a Dual-Spool, Separate-Exhaust
  • Jet Engines-Powering Modern Airplanes
  • The GE90 - an Introduction
  • Thermodynamic and Aerodynamic Analysis of an Air-Driven Fan System in Low-Cost High-Bypass-Ratio Turbofan Engine
  • NASA ___N,,,G ,I LANGLERESEARCHY CENTER LIBRARYNASA HAMPTONVIRGINIA
  • Exchange Rate Analysis for Ultra High Bypass Ratio Geared Turbofan Engines
  • Specifications
  • NASA FAP SFW Core Noise
  • Tf34 Turbofan Quiet Engine Study
  • 94-Inch High-Bypass Turbofan Engine
  • N94-25708 General Descriptions of the Structures, Weight and Balance, Stability and Control, Performance, and Engine Design
  • A Brief Study of the Effects of Turbofan-Engine Bypass Ratio on Short- and Long-Haul Cruise Aircraft
  • TECHNICAL REPORT on Propulsion System and Auxiliary Power Unit (APU) Related Aircraft Safety Hazards


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