could you help me with a methods of thermal cycle analysis of swirl range extender MGTs supported by turbocharger,  Including a intercooler recuperator model with effectiveness equations to use for calculating the  enthalpy of formation, and other relevant thermodynamic properties of hydrogen at various temperatures. the flame behavour as using swirl. This will involve equation of: Compressor: Calculate the outlet temperature and enthalpy of the compressed air using compressor efficiency and isentropic relations. Combustor : Assuming no heat loss, calculate the product temperature and enthalpy after combusting hydrogen with air. Fuel Processor (for hydrogen system): Model the process of converting hydrogen into a high-temperature gas stream suitable for the turbine. This might involve equations for enthalpy change during dissociation and subsequent reactions. Turbine: Calculate the outlet temperature and enthalpy of the expanded gas using turbine efficiency and isentropic relations. Recuperator (if applicable): Model the heat exchange between the hot exhaust stream and the compressed air using effectiveness or capacitance methods. please try your best to help as i need to start working on my project. thank you for all your efforts as you have been amazing helping me during this year. really appreciat it.