Assertion: turbine's rotor | /r/HasProperty | the one
Facets:
Source sentences:
text: The first one is the thrust coefficient of the rotor, which is the one which should be corrected for high rotor loading (i.e., for high values of a {\displaystyle a} ), while the second one ( c t {\displaystyle c_{t}} ) is the tangential aerodynamic coefficient of an individual blade element, which is given by the aerodynamic lift and drag coefficients.