turbines are much harder to size, because theres no clear cut relationship between A/R and shaft rotational speed (from what ive read). you cant just say "if your engine needs ___ lb/m of boost to maintain ____ psi, the rotational speed with ___ compressor means the shaft goes ____ RPM and you need ____ A/R on the turbine".
so much comes into play with VE and airspeed velocity its impossible to calculate empiracally. things that happen in the manifold have a big impact on the A/R... from what ive read, everything says you can only ballpark A/R or go on experience. things like the backpressure created by the bearing resistance versus the forward flow out of the head/manifold... its just two forces working totally opposite one another
so much comes into play with VE and airspeed velocity its impossible to calculate empiracally. things that happen in the manifold have a big impact on the A/R... from what ive read, everything says you can only ballpark A/R or go on experience. things like the backpressure created by the bearing resistance versus the forward flow out of the head/manifold... its just two forces working totally opposite one another