Air Intakes - Aircraft Gas Turbine Engines #04

[@alex458897]

Thank you for this high quality content!

[@rudyandersson39STAR]

I didn't know how many parts there was such as the spike . Thumbs up for the explained

[@ChrisZoomER]

Brilliant explanation. The only thing you missed is that many other high-bypass engines have a convergent inlet to maximize "ram intake" in order to slow the airflow down to Mach 0.5 when a jetliner is cruising at transonic speeds.

[@owouwu9032]

With the sr71 the bypass wasn’t from the intake but it was from the 6th stage of the compressor directly to the afterburner

[@anubhavparihar5706]

Nice work

[@mohammedpilot2335]

Thanks

[@natigahmet1903]

Well explained, but sometimes need to make a stress on that stall and stonewall absolutely different phenomena

[@thomashvnmusic]

Thank you!

[@aeroair6555]

You're welcome!

[@martinmilev611]

Perfect

[@gazmchurcty7485]

Can someone explain the stages of compression?

[@gabrielibarcena7481]

lol @ 12:53

[@aqumant]

Why does it auto-generate Dutch subtitles?? Just why :D