My Mechanical Design Project

viscouz23 · September 28, 2019, 06:57

Hi everyone , ım a mechanical engineering 4th graduate student.Also ı took the project about gas turbine blade stress analysis.I need some articles,books and helpful resource about it.Do you have any suggest about it ı want to know that.Thanks for reading

viscouz23 · September 28, 2019, 14:47

Quote:

Originally Posted by viscouz23

Hi everyone , ım a mechanical engineering 4th graduate student.Also ı took the project about gas turbine blade stress analysis.I need some articles,books and helpful resource about it.Do you have any suggest about it ı want to know that.Thanks for reading

Any suggests?

AtoHM · September 30, 2019, 01:22

You need to add some specific details of what you are trying to do. You mentioned stress analysis. If you are not planning to perform FSI calculations, you are probably in the wrong forum, because this is a cfd forum.

There is an indefinite amount of publications and papers on gas turbines so you need to specify what exactly it is you need help to find. I know for a fact that you will have a hard time grabbing some real industry in-duty turbine blade geometry to perform calculations on. They are kept secret for obvious reasons.

viscouz23 · September 30, 2019, 18:07

Quote:

Originally Posted by AtoHM

You need to add some specific details of what you are trying to do. You mentioned stress analysis. If you are not planning to perform FSI calculations, you are probably in the wrong forum, because this is a cfd forum.

There is an indefinite amount of publications and papers on gas turbines so you need to specify what exactly it is you need help to find. I know for a fact that you will have a hard time grabbing some real industry in-duty turbine blade geometry to perform calculations on. They are kept secret for obvious reasons.

I understood you.Sorry it is my fault.I have a mechanical design project about turbine blade stress analysis , ı would like to know general knowledge of turbine blades,blade design and cfd analysis knowledge about those blades.Because ı would calculate stress on blades and ı need to know rotational motion , air intakes on blades with high speed(less than 1 mach) how it affects on blade stress.I tried to explain ı hope you understand

AtoHM · October 1, 2019, 12:08

Yes, but its still unclear what you are asking. Is something wrong with the stuff you can find on the internet? There are great books on turbomachinery where you will find all the mentioned basics. Also I assume you are subscribed to a university and have much easier access to papers from IEEE or ASME for example.

September 28, 2019, 06:57	My Mechanical Design Project	#1
viscouz23 New Member Mehmet Cetin Join Date: May 2019 Location: Istanbul Posts: 11 Rep Power: 6	Hi everyone , ım a mechanical engineering 4th graduate student.Also ı took the project about gas turbine blade stress analysis.I need some articles,books and helpful resource about it.Do you have any suggest about it ı want to know that.Thanks for reading

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September 30, 2019, 01:22		#3
AtoHM Senior Member M Join Date: Dec 2017 Posts: 642 Rep Power: 12	You need to add some specific details of what you are trying to do. You mentioned stress analysis. If you are not planning to perform FSI calculations, you are probably in the wrong forum, because this is a cfd forum. There is an indefinite amount of publications and papers on gas turbines so you need to specify what exactly it is you need help to find. I know for a fact that you will have a hard time grabbing some real industry in-duty turbine blade geometry to perform calculations on. They are kept secret for obvious reasons.

October 1, 2019, 12:08		#5
AtoHM Senior Member M Join Date: Dec 2017 Posts: 642 Rep Power: 12	Yes, but its still unclear what you are asking. Is something wrong with the stuff you can find on the internet? There are great books on turbomachinery where you will find all the mentioned basics. Also I assume you are subscribed to a university and have much easier access to papers from IEEE or ASME for example.