I am quite new to turbochargers and am researching a project that involves the use of turbochargers. I have a question about the force generated on the compressor outlet. We understand the exhaust gas directed into the turbine side of the turbocharger, which in turn spins the shaft wheel, and the residual exhaust gas exits the outlet of the turbine. So when the shaft spins, it also drives the compressor wheel which sucks in and compresses the air, and pushes it out of the compressor outlet back into the car engine.
My question is, when this compressed air exits the compressor outlet, is the force or thrust of this airflow, same as the force/thrust of the exhaust gas exiting the turbine outlet, since the shaft is working both the turbine and compressor wheel simultaneously? And can the force/thrust at the compressor outlet be adjusted to be less, same or more than the force/thrust generated at the turbine outlet?