Thermodynamic Performance and Creep Life Assessment Comparing Hydrogen- and Jet-Fueled Turbofan Aero Engine by Emmanuel O. Osigwe, Arnold Gad-Briggs, Theoklis Nikolaidis, Soheil Jafari, Bobby Sethi, Pericles Pilidis

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Techno-environmental assessment of a hydrogen-fuelled combined-cycle gas turbine for a liquid hydrogen tanker by Abdullah NFNR Alkhaledi, Amit Batra, Suresh Sampath, Pericles Pilidis

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Techno-Environmental Mission Evaluation of Combined Cycle Gas Turbines for Large Container Ship Propulsion by Abdulaziz M. T. Alzayedi, Amit Batra, Suresh Sampath, Pericles Pilidis

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TERA of Gas Turbine Propulsion Systems for RORO Ships by Abdulaziz M. T. Alzayedi, Abdullah N. F. N. R. Alkhaledi, Suresh Sampath, Pericles Pilidis

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Turboelectric Uncertainty Quantification and Error Estimation in Numerical Modelling by Mosab Alrashed, Theoklis Nikolaidis, Pericles Pilidis, Soheil Jafari

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Exchange Rate Analysis for Ultra High Bypass Ratio Geared Turbofan Engines by Theoklis Nikolaidis, Soheil Jafari, David Bosak, Pericles Pilidis

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Techno-Environmental Evaluation of a Liquefied Natural Gas-Fuelled Combined Gas Turbine with Steam Cycles for Large Container Ship Propulsion Systems by Abdulaziz M. T. Alzayedi, Suresh Sampath, Pericles Pilidis

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Techno–Economic and Risk Evaluation of Combined Cycle Propulsion Systems in Large Container Ships by Abdulaziz M. T. Alzayedi, Suresh Sampath, Pericles Pilidis

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An Iterative Method to Derive the Equivalent Centrifugal Compressor Performance at Various Operating Conditions: Part I: Modelling of Suction Parameters Impact by Waleed Albusaidi, Pericles Pilidis

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Energetic and Exergetic Analysis of Combined Cycle Power Plant: Part-1 Operation and Performance by Abdulrahman Almutairi, Pericles Pilidis, Nawaf Al-Mutawa

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‘Greening’ an Oil Exporting Country: A Hydrogen, Wind and Gas Turbine Case Study by Abdulwahab Rawesat, Pericles Pilidis

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Performance assessment of simple and modified cycle turboshaft gas turbines by Barinyima Nkoi, Pericles Pilidis, Theoklis Nikolaidis

“…In course of carrying out this research, turbomatch software established at Cranfield University based on gas turbine theory was applied to conduct simulation of a simple cycle (baseline) two-spool helicopter turboshaft engine model with free power turbine. …”
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