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Nimonic

  • Capabilities of Midlands Aerospace Companies 2010-2011 Midlands Capability for the World’S Aerospace Industry

    Capabilities of Midlands Aerospace Companies 2010-2011 Midlands Capability for the World’S Aerospace Industry

  • Capabilities of Midlands Aerospace Companies

    Capabilities of Midlands Aerospace Companies

  • High Temperature Parts

    High Temperature Parts

  • Examination of Material Variation on the Life of Gas Turbine Backing-Up Renewable Energy Sources

    Examination of Material Variation on the Life of Gas Turbine Backing-Up Renewable Energy Sources

  • Superalloys for High Temperatures—A Primer

    Superalloys for High Temperatures—A Primer

  • Examination of Material Variation on the Life of Gas Turbine Backing-Up Renewable Energy Sources

    Examination of Material Variation on the Life of Gas Turbine Backing-Up Renewable Energy Sources

  • Materials for Gas Turbines – an Overview

    Materials for Gas Turbines – an Overview

  • Metropolitan Vickers, the Gas Turbine, and the State: a Socio

    Metropolitan Vickers, the Gas Turbine, and the State: a Socio

  • Analytical Comparative Study of Gas Turbine Blade Materials

    Analytical Comparative Study of Gas Turbine Blade Materials

  • Superalloys, the Most Successful Alloy System of Modern Times-Past, Present, and Future

    Superalloys, the Most Successful Alloy System of Modern Times-Past, Present, and Future

  • The Development of the Whittle Turbojet

    The Development of the Whittle Turbojet

  • Research Memorandum

    Research Memorandum

  • Oxidation Behavior of Two Nickel-Base Superalloys Used As Elevated Temperature Valves in Spark Ignited Engines and Diesel Exhaust Recirculation (Egr) Applications

    Oxidation Behavior of Two Nickel-Base Superalloys Used As Elevated Temperature Valves in Spark Ignited Engines and Diesel Exhaust Recirculation (Egr) Applications

  • Nickel Chromium Cobalt Alloys

    Nickel Chromium Cobalt Alloys

  • Rejuvenation of Used Turbine Blades by Hot Isostatic Processing 57

    Rejuvenation of Used Turbine Blades by Hot Isostatic Processing 57

  • INSG Insight INSG SECRETARIAT BRIEFING PAPER April 2013 – No.20

    INSG Insight INSG SECRETARIAT BRIEFING PAPER April 2013 – No.20

  • Nickel Chromium Superalloy

    Nickel Chromium Superalloy

  • Circular of the Bureau of Standards No. 509: Bibliography of Books and Published Reports on Gas Turbines, Jet Propulsion, and Ro

    Circular of the Bureau of Standards No. 509: Bibliography of Books and Published Reports on Gas Turbines, Jet Propulsion, and Ro

Top View
  • Modelling and Simulation of Gas Turbine Blade with Different Geometrical Perforated Holes and Blade Materials: Software Analyses
  • The Historical Evolution of Turbomachinery
  • Royal Air Force Historical Society Journal 53
  • Fabrication and Characterization of the Newly Developed Superalloys Based on Inconel 740
  • Corrosion-Fatigue Failure of Gas-Turbine Blades in an Oil and Gas Production Plant
  • A History of Superalloy Metallurgy for Superalloy Metallurgists
  • High Temperature Alloys for the Htgr Gas Turbine: Required Properties and Development Needs
  • Circular of the Bureau of Standards No. 482: Bibliography of Books And
  • Wear Characteristics of Superalloy and Hardface Coatings in Gas Turbine Applications–A Review
  • Attachment Methods Fig 5A Turbine Blade Attachment - Fir-Tree Root
  • Review on Mechanical Thermal Properties of Superalloys and Thermal Barrier Coating Used in Gas Turbines
  • Electron Beam Cold Hearth Refinement Processing of Inconel
  • Estimating of Gamma Phase Composition in Nickel-Base
  • High Temperature Corrosion by Combustion Gases Produced by Burning Liquid Fuels Containing Sulphur, Sodium and Vanadium


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