Which blade generates more thrust on the T-6B during a climb when PCL is advanced?

In the context of the T-6B during a climb with the power control lever (PCL) advanced, the left upgoing blade generates more thrust.

When the aircraft is in a climb, the rotational direction of the propeller combined with the angle of attack for each blade affects thrust generation. As the left blade moves up and the right blade moves down, the upgoing blade benefits from a higher angle of attack as it enters relative wind, thus producing greater lift and thrust compared to the downgoing blade, which experiences a lower angle of attack due to the airflow direction.

As the PCL is advanced, the increased power further enhances the performance of the upgoing blade, making it more effective in generating thrust. This characteristic is crucial in terms of performance during climbs, where maximizing thrust from each blade is essential for optimal climb rate.

In summary, the left upgoing blade's advantageous position and increased angle of attack when the aircraft is climbing contribute to its ability to generate more thrust in this scenario.