Aerospace Thermodynamics Analysis
Budget: ₹600 – ₹1,500 INR
You are working as an Aeronautical Engineer in the Research and Development (R&D) division of an engineering
company. Your line manager has assigned you the task of evaluating the behaviour of gases and fluids in different
thermodynamic systems used in aerospace applications and assessing their thermodynamic performance.
In this assignment, you will analyse two engineering systems:
1. A closed-system heat engine (Stirling engine)
2. An open-system heat exchanger
Your objective is to investigate how these systems operate, evaluate their thermodynamic behaviour, and assess their
performance using relevant thermodynamic principles and calculations. You are required to prepare an individual
technical engineering report that clearly presents and communicates your findings using appropriate technical
language.
You are required to apply the concepts, relevant diagrams, and analytical methods discussed and practiced in class.
Your report should include explanations supported by calculations, diagrams, tables, figures, and relevant engineering
discussion to justify your analysis of the two thermodynamic systems.
company. Your line manager has assigned you the task of evaluating the behaviour of gases and fluids in different
thermodynamic systems used in aerospace applications and assessing their thermodynamic performance.
In this assignment, you will analyse two engineering systems:
1. A closed-system heat engine (Stirling engine)
2. An open-system heat exchanger
Your objective is to investigate how these systems operate, evaluate their thermodynamic behaviour, and assess their
performance using relevant thermodynamic principles and calculations. You are required to prepare an individual
technical engineering report that clearly presents and communicates your findings using appropriate technical
language.
You are required to apply the concepts, relevant diagrams, and analytical methods discussed and practiced in class.
Your report should include explanations supported by calculations, diagrams, tables, figures, and relevant engineering
discussion to justify your analysis of the two thermodynamic systems.