The air enters the air intake pipe at the front face of the air intake, not at the S shaped bend,
then it only rushes in through the air pipe through a smooth passage of S shaped intake ,
and with the aid of great suction pull from the engine blades, without friction as it is the property of the fluids,
Even at a higher AOA the air that enters through the air intake at the front will compress the air to the engine with no interference from S shaped bend,
Even 4th gen Rafale and many other fighters have bends in air intake ,
with the stated intention of RCS reduction as primary objective ,
and it does not seem to critically affect their high AOA performance,
The job of the S shaped air intake designers is to ensure enough air to the engine considering all the high AOA phases , by designing it with such dimensions suitably.
It is not needed for normal fighters, but the primary goal of 5th gen fighters is nil exposure of engine blades to the enemy radar, as the exposure of any minute portion will result in the fighter being tracked by ever increasingly powerful x band radars.
So until now all 5th gen fights except PAKFA followed this route,
If not a full S Shape then just a bend like the RAFLE could have avoided the cumbersome radar blocker, which cannot be as stealth compliant as S Shaped air intake.
IF ADA follows the same route for AMCA,
saying the russain example of maneuverability and supply of more air at critical AOA maneuvers,
takes precedence over more stealthy S shaped air intake ,
will it be acceptable for IAF?
By the same analogy radar blockers always interfere with air flow into air intake and their effect on the fighter during critical AOA phase is even more .