AERO737

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@Auday365 24 күн бұрын

One of the best videos in this field, very extensive in details, well narrated, and useful to all.

@MugeSam-vy7ne 6 ай бұрын

Appreciated 🙏🙏

@Manpromec Жыл бұрын

I want to design and manufacture a small jet engine with 80lb thrust, what book do you recommend I study? I am from Peru

@mrgreyman3358 Жыл бұрын

This is an excellent tutorial, especially as I am just starting to study aircraft engineering after retiring from the military. Thank you for this.

@rohanbaty3155 Жыл бұрын

Where is part 2 silvous plait?

@danranquist502 Жыл бұрын

Im listening..without watching i was able to puck up on the fact that professional terminology is important yet not all that difficult to understand. Thanks for the content !

@Adolf_Meowtler Жыл бұрын

Turbine jet engines have less moving parts than piston engines. Turbine jet engines:

@christopherk9093 Жыл бұрын

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 KZfaq 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 kzfaq.info/get/bejne/hreBhriWnNK8Y6d6.htmlas Turbines Engines-Part 3:Compressors YVO

@loveworthkaba9870 Жыл бұрын

Awesome project, where can I get the parts

@raccoonair Жыл бұрын

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%.

@raccoonair Жыл бұрын

Excellent; thank you for posting.

@dovydenaspdx 2 жыл бұрын

The verbal descriptions are incredibly good and simple. Statement of fact followed by conclusion, no babbling.

@spvmentors7258 2 жыл бұрын

Very nicely explained. Thanks.

@entertainerclub8069 2 жыл бұрын

Awesome , can you explain the combustion chamber

@entertainerclub8069 2 жыл бұрын

Awesome , can you explain the combustion chamber

@MaxisMBQ 2 жыл бұрын

thank you

@user-px8eo9vw2j 2 жыл бұрын

جميل نبي علم زائدة جزاك الله خيرا علم

@infidel6347 2 жыл бұрын

Awesome , can you explain the combustion chamber

@grahamj9101 2 жыл бұрын

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'.