Procedures

Inverse cosine of x, result in degrees

Inverse sine of x, result in degrees

Inverse tangents of y/x (see atan2d), result in degrees

Inverse tangents of x, result in degrees

Find root of a function in an interval using bisection.

This interface is used to initialize the boundary_conditions_t

Cosine of x in degrees

This subroutine creates the mesh data structure.

This subroutine creates a performance model object based on the type specified in the toml configuration file. The performance model type is read from the toml configuration file and the appropriate constructor function is called to create the performance model object.

Load the configuration file and create the tfana_job_t object.

Create a thermodynamic model from the configuration file.

Cross product in R3

Create a new curve from a sequence of points.

Conversion from degrees to radians

Approximate the derivative of a function using finite differences

Approximate the second derivative of a function using finite differences

Initialize the flow field structure and set all fields to zero

Returns the integral of f with respect to x using integrated Taylor expansion f: array of f values x: array of x values returns: the integral of f with respect to x

Compute the intersection of two curves.

Reads the machine description from a TOML table

Compute the mass flow rate through a quasinormal

Find root of a function using Newton’s or secant method.

Standard L2 norm of a vector

Standard L2 norm of a vector squared

Outer product

Returns the integral of f with respect to x using integrated Taylor expansion f: array of f values x: array of x values returns: the integral of f with respect to x

Prints a brief help message

Project a point onto a curve.

Conversion from radians to degres

Create a new ramp function with given start, duration, y1 and y2

This subroutine recalculates the mesh parameters (streamline angles, curvatures, etc.)

This subroutine redistributes the streamlines along a quasinormal.

Find root of a function using given method

Save the flow field to a Matlab/Octave compatible file

Sine of x in degrees

Tangents of x in degrees

Update the state variables at the given quasinormal from the total enthalpy, entropy and velocity components.

Compute the tangential velocity. The rotating frame is taken into account for leading and trailing edge of rotors. Similarly, mirroring is taken into account for compressor stators and turbine rotors.