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Overall pressure ratio

  • Aerospace Engine Data

    Aerospace Engine Data

  • High Pressure Ratio Intercooled Turboprop Study

    High Pressure Ratio Intercooled Turboprop Study

  • Helicopter Turboshafts

    Helicopter Turboshafts

  • Improving Engine Efficiency Through Core Developments

    Improving Engine Efficiency Through Core Developments

  • Download This Issue (PDF)

    Download This Issue (PDF)

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

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

  • Pzl-10 Turboshaft Engine – System Design Review

    Pzl-10 Turboshaft Engine – System Design Review

  • Conceptual Design of a Turbofan Engine for a Supersonic Business Jet

    Conceptual Design of a Turbofan Engine for a Supersonic Business Jet

  • Etu – V Tulpar

    Etu – V Tulpar

  • ITU Beengine for a Next Generation Trainer

    ITU Beengine for a Next Generation Trainer

  • 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

  • Military Jet Engine Acquisition

    Military Jet Engine Acquisition

  • Simulating Indirect Thrust Measurement Methods for High

    Simulating Indirect Thrust Measurement Methods for High

  • Performance Enhancement of Microturbine Engines Topped With

    Performance Enhancement of Microturbine Engines Topped With

  • Solve Problems – Ideal Cycle Analysis of Air Breathing Engines

    Solve Problems – Ideal Cycle Analysis of Air Breathing Engines

  • Simulation and Performance Analysis of Ejector Nozzle In

    Simulation and Performance Analysis of Ejector Nozzle In

  • 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
  • Let's Re-Engine the Concorde!
  • Innovative Double Bypass Engine for Increased Performance
  • Analysis of the Effects of Methane Ingestion on Turboshaft Engines
  • Supersonic Technology Concept Aeroplanes for Environmental Studies
  • GE Aviation Cincinnati, Ohio
  • Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project
  • Jet Engines-Powering Modern Airplanes
  • The GE90 - an Introduction
  • Pratt & Whitney PW1000G
  • Full Length Review Article DEVELOPMENT RESEARCH
  • 4. Specific Fuel Consumption 36 5
  • SF-1600: a Next Generation High Efficiency Turboprop for Single- Engine Aircraft Design Team: Elliot Bicker # 531124 ______
  • Candidate Engine for a Next Generation Supersonic Transport
  • Wj-25 Design Prposal
  • Making Turbofan Engines More Energy Efficient
  • Performance Prediction and Simulation of Gas Turbine Engine Operation (La Pr´Evision Des Performances Et La Simulation Du Fonctionnement Des Turbomoteurs)
  • Turbojet, Turbofan and Variable Cycle Engines for High Speed Propulsion
  • Analysis of an After Burner in a Jet Engine


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