There is a lot of love in the design of one of these hair driers. Makes me feel very good in witnessing through these nicely produced TH-cam Videos. Already I am in admiration those who find a way to study and work with such engine poetry. It almost feels like each working turbine is a laboratory in the study of air vapor under pressure and fluids. Thank You AERO737 th-cam.com/video/PQQSUe7lX3sG/w-d-xo.htmlas Turbines Engines-Part 3:Compressors YVO
I have just found this series of videos and my initial reaction is positive. However, the term 'compression ratio' applies to internal combustion engines and it is actually a volume ratio. The correct term for a gas turbine engine is 'pressure ratio'.
Compression ratio is the ratio of two volumes whereas the pressure ratio is the ratio of two pressures. Gas Turbine is also an Internal Combustion Engine.
One of the best videos in this field, very extensive in details, well narrated, and useful to all.
The verbal descriptions are incredibly good and simple. Statement of fact followed by conclusion, no babbling.
An excellent tutorial, thanks for sharing I have learn the principal 30 years ago but still fascinate me to see and hear about it.
Can gggnvyipphtrrrryppo
This is an excellent tutorial, especially as I am just starting to study aircraft engineering after retiring from the military. Thank you for this.
Excellent video. One of the best I've seen. I'm learning all kinds of stuff.
There is a lot of love in the design of one of these hair driers. Makes me feel very good in witnessing through these nicely produced TH-cam Videos. Already I am in admiration those who find a way to study and work with such engine poetry. It almost feels like each working turbine is a laboratory in the study of air vapor under pressure and fluids. Thank You AERO737 th-cam.com/video/PQQSUe7lX3sG/w-d-xo.htmlas Turbines Engines-Part 3:Compressors YVO
I have just found this series of videos and my initial reaction is positive. However, the term 'compression ratio' applies to internal combustion engines and it is actually a volume ratio. The correct term for a gas turbine engine is 'pressure ratio'.
Compression ratio is the ratio of two volumes whereas the pressure ratio is the ratio of two pressures. Gas Turbine is also an Internal Combustion Engine.
Wonderful video. The best one on youtube.
Again excellent, it's great we have FADEC now. If I may, a small mistake at 12:00, the green line engine RPM should be 105, not 60%.
Very nicely explained. Thanks.
This really helped me building my own jet engine
Very Good insight
Any update on chapter 14? Need to see fuel systems
Explain very well
Excellent.. really
where can I get this software from?
Appreciated 🙏🙏
جميل نبي علم زائدة جزاك الله خيرا علم
thank you
AERO737 waiting for new videos
Awesome , can you explain the combustion chamber
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please share with us the rest of systems
Awesome , can you explain the combustion chamber
Awesome , can you explain the combustion chamber