What are some recommended resources for learning about gas turbine aero design?

AI Thread Summary
A user is preparing for a new role in Aero CFD at a power generation gas turbine company and seeks recommendations for foundational reading on aero design. They mention a specific textbook but are unsure if it is a definitive resource. Discussion highlights the importance of covering modern concepts like intercooling and recuperation in turbine design. Additionally, the conversation notes the significant power output of advanced gas turbines, such as GE's H-series, which can produce 480 megawatts. The insights emphasize the complexity and scale of gas turbine technology in power generation.
minger
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Hello gas turbine peeps,

I'm going to be starting a new position doing Aero CFD for a power generation gas turbine company. While I have a good amount of theoretical and academic knowledge of CFD in general, my practical application experience is limited.

I was hoping to do a little light reading on aero design of these things in the next few weeks before I show up. I have seen this guy:
https://www.amazon.com/dp/013015847X/?tag=pfamazon01-20

but not sure if there are any others that are referred to as "bibles" of the field. If anyone has any other thoughts, I'd appreciate it. Thanks,
 
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Well, my only thought is that any time a textbook is over $100, it's either pretty good or extremely overrated.

As a guide, if they're not discussing both intercooling and recuperation, they're behind the times. Ideally, a turbine will develop both infinate pressure as well as exit temps equaling inlet temps. Practically, that's just a tad difficult, as things are close to melting during the compressor/combustor stages.

This is of course for jet engines. For steam turbines (you did mention "power generation" did you not?) things are a bit different, unless by "gas turbine" you mean a turbine fueled by natural gas.

As for a "little light reading," you might wish to aquaint yourself with GE's series of power generation gas turines. Their H-series is rather formidible, and enjoys 480 megawatts of supercomputing power (actually power production) which went into its design. More http://gepower.com/prod_serv/products/gas_turbines_cc/en/h_system/index.htm" .

By the way, this is neither a small nor inexpensive unit. It's output far exceeds that of any jet engine. 480 MW is roughly equivalent to well over half a million horsepower.
 
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Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
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