CircularFillet: Method to find maximum fillet radius between two curves.
BladeFillet: New fillet functionalities specifically designed for blade fillets. It can handle constant radius and variable radius values and offers a method to not cross specified boundary curves.
BladeFillet: Feature to calculate maximum constant fillet radius between two blades.
BladeThickness: Object for the turbo machine workflow, handling the creation of thickness distributions.
BRep Intersect and Trim: Now works with FPlane.
BReps: Added option to set transparency for individual faces.
Calculate Meridional Value: Function to calculate m or m’ from a meridional contour based on the t-position.
Dimensionality Reduction: New and better back-transformation.
Extract Mean Camber Surface: Function to extract the camber surface based on faces of pressure and suction side.
FAirfoilBlade: New object to conveniently create 3D blades based on 2D airfoil or hydrofoil definitions.
FBlade: Object for turbo machine workflow, handling and organizing the creation of the component blade.
FBladeCamber: Object for the turbo machine workflow, handling the creation of angle distributions, camberlines and cambersurfaces.
FBladedComponent: Object for turbo machine workflow, handling the creation of a component with blades.
FMeridionalContours: Object for the turbo machine workflow, handling the meridional contours of the blade
FTurboMachine: New workflow, to create turbo machines in a streamlined and fast way.
FUnbladedComponent: Object for turbo machine workflow, handling the creation of a component without blades.
FVector3: New command to calculate the wrap angle / theta angle of a vector / point in a cylindrical coordinate system: FVector3.getCylinderCoordsAngle().
FVector3: New command to calculate the radius of a vector / point in a cylindrical coordinate system: FVector3.getCylinderCoordsRadius().
Import BladeGenRTZT: Feature to import BladeGen RTZT files.
Import GeomTurbo: Feature to import GeomTurbo files.
Import Turbo Design: Feature to import Turbo Design files.
Inverse Cylinder Transformation: Added function to transform 3D profiles with inverse cylinder transformation into the 2D x,y-plane.
Meridional Area Distribution: Function to calculate the meridional area distribution, returned as a curve in the x,y-plane.
Propeller Calculator: Feature to calculate propeller properties based on specified operation conditions.
Sample: New Sample of an axial compressor stator blade based on “TU Berlin TurboLab Stator”.
Sample: New Sample of a centrifugal pump, designed with the turbo machine workflow.
Sample: Added sample for a radial turbine modeled with the turbo machine workflow, including scallops and variable radius fillets.
Transform to Meridional Plane: Simple function to transform a 3D camberline into the meridional plane.
Triangulation: Included a higher accuracy switch for triangulation (optional) for difficult cases.
Turbo Blade Analysis: Function to calculate beta and theta angle distributions from imported or modeled blades and cambersurfaces.
Turbo Section Analysis: Function to calculate beta and theta angles distribution from a camberline.
Types: Added Type FXml for parsing and writing XML files.
Types: Added Type FComplex for calculations involving complex numbers.