turbo_moc.geometry.linear_cascade module

Physical planar cascades using the same blade-to-blade mesh as annular rows.

The numerical plane retains pitchwise q_x and downstream-negative q_y. Unlike the annular conformal chart, both coordinates are physical lengths: X = -q_y, Y = q_x, Z = eta * blade_height. No reference radius is needed.

class turbo_moc.geometry.linear_cascade.LinearCascadeDefinition(meridional_chord: float, blade_height: float, pitch: float)

Bases: object

Methods

to_dict

blade_height: float

meridional_chord: float

pitch: float

to_dict()

class turbo_moc.geometry.linear_cascade.LinearCascadeMapping(definition)

Bases: object

Identity blade sections extruded between two parallel span endwalls.

Methods

meridional_points(u, eta, *[, derivative])	Return (span height, streamwise distance) for the meridional plot.
periodic_transform()	Homogeneous translation from periodic_left to periodic_right.
section_scale(eta)	Every span station has the same physical profile and pitch.

map_points

is_linear = True

map_points(q, eta)

meridional_points(u, eta, *, derivative=False)

Return (span height, streamwise distance) for the meridional plot.

orientation = 1

periodic_transform()

Homogeneous translation from periodic_left to periodic_right.

section_scale(eta)

Every span station has the same physical profile and pitch.

turbo_moc.geometry.linear_cascade.build_linear_section(nozzle, config, template)

Scale the fitted blade and its MoC-derived pitch together to the chord.

Preserving pitch/chord avoids introducing an independent, unstated solidity choice. The sole automatic passage-placement search remains in 2D.