Abstract: A turbine vane for a gas turbine engine with an airfoil portion including a perimeter wall having first, second, and third sets of cooling holes defined therethrough, including the holes numbered HA-1 to HA-13, HB-1 to HB-13 and PA-1 to PA-9, respectively, and located such that a central axis thereof extends through the respective point 1 and point 2 having a nominal location in accordance with the X, Y, Z Cartesian coordinate values set forth in Table 3.

Abstract: A turbine vane for a gas turbine engine with an airfoil portion including a perimeter wall having first, second, and third sets of cooling holes defined therethrough, including the holes numbered HA-1 to HA-13, HB-1 to HB-13 and PA-1 to PA-9, respectively, and located such that a central axis thereof extends through the respective point 1 and point 2 having a nominal location in accordance with the X, Y, Z Cartesian coordinate values set forth in Table 3.

Abstract: A method of processing text is provided, in which each word or sequence of words is checked against a lexicon of words and sequences of words each having, associated therewith a score on at least one personality scale, which can be a multi-dimensional scale for representing various personality traits. These scores are then compared against a target personality, and, if the score has a predetermined degree of mismatch with the target personality, a word or sequence of words with a similar semantic content but a better matching score on the personality scale is retrieved.