Post by aero on Apr 9, 2024 20:29:07 GMT -5
aero Avatar
Apr 10, 2024 3:29:07 GMT 2 aero said:
I'm working on our graduation project, and we need to design a micro jet engine. However, I'm having trouble finding clear guidance on the equations needed to design the combustion chamber. If you can help me out with resources, I'd greatly appreciate it.
My project involves designing a microjet engine to be mounted on an RC airplane. We're constrained by a specific design point which is mass flow rate =0.3 kg/s . The challenge lies in starting the design of the combustion chamber. I have information on the mass flow rate and maximum temperature, but I'm unsure how to divide the combustion chamber into primary, secondary, and tertiary zones, as well as determining the size of the holes. If anyone has experience in this area and can guide me through the process, I would be extremely grateful. I'm eager to finish my graduation project and tired of spending days reading vague and non-specific textbooks.
I need some help finding equations or reliable rules. Despite checking numerous references on gas turbine theory, I haven't found any useful ones.
Apr 10, 2024 3:29:07 GMT 2 aero said:
I'm working on our graduation project, and we need to design a micro jet engine. However, I'm having trouble finding clear guidance on the equations needed to design the combustion chamber. If you can help me out with resources, I'd greatly appreciate it.
My project involves designing a microjet engine to be mounted on an RC airplane. We're constrained by a specific design point which is mass flow rate =0.3 kg/s . The challenge lies in starting the design of the combustion chamber. I have information on the mass flow rate and maximum temperature, but I'm unsure how to divide the combustion chamber into primary, secondary, and tertiary zones, as well as determining the size of the holes. If anyone has experience in this area and can guide me through the process, I would be extremely grateful. I'm eager to finish my graduation project and tired of spending days reading vague and non-specific textbooks.
I need some help finding equations or reliable rules. Despite checking numerous references on gas turbine theory, I haven't found any useful ones.
