Safran Aircraft Engines

Jean-Armand Marc Emilien Destouches

Ludovic Pintat

Guillaume Jochen Scholl

Thomas Michel Julien Mervant

Pascal Pierre Nicolas Routier

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y, Zadim given in Table 1, in which the coordinate Zadim is the quotient D/H where D is the distance of the point under consideration from a first reference plane Psituated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.

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Savigny-Le-Temple, France

Jean-Armand Marc Emilien Destouches