J-20 5th Gen Fighter Thread VIII

sometimesnaive

New Member
Registered Member
That’s called differential thrust. We’ve seen this happen numerous times both in the air and prior to takeoff.
I am aware, although it just doesn't seem all that practical to the best of my knowledge, especially since the moment arm would be quite small on J-20 compared to fighters with wider spaced engines/shorter fuselages. Assuming WS-15 spools fast, I don't know why differential thrust would be used especially given rudders seem like a much superior option even at low airspeed, unless its digital. What am I missing here?
 

Atomicfrog

Major
Registered Member
Some people are still gonna complain about ventral strakes, but they serve an important purpose maintaining stability at high AOA because of how small the all-moving slabs are.
Also hide the engine nozzles from the sides. Beside small updates, I dont see further big evolution on the J-20 platform with the sixth generation fighters coming along.
 
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Alfa_Particle

Senior Member
Registered Member
I am aware, although it just doesn't seem all that practical to the best of my knowledge, especially since the moment arm would be quite small on J-20 compared to fighters with wider spaced engines/shorter fuselages. Assuming WS-15 spools fast, I don't know why differential thrust would be used especially given rudders seem like a much superior option even at low airspeed, unless its digital. What am I missing here?
Afaik pilots do actively use differential thrust in crosswind conditions during landing. See:
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slithly

Just Hatched
Registered Member
if this has already been posted or asked feel free to delete, i couldnt find it within 50ish pages 1776196808361.png
seems like there are differences between the intakes on the j20. adding a diverter to a diverterless supersonic intake? the bump itself seems to have also changed shape. any ideas?
 
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