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An API for working with Bladed Next Gen models.

Project description

Bladed Next Gen Python Models API

dnv_bladed_models=0.4.0

A Python package to easily work with JSON input models for Bladed Next Generation.

Visit https://bladednextgen.dnv.com/ for more information.

Prerequisites

  • Requires Python 3.7 or above

Usage

Add import

import dnv_bladed_models as models

There are a large number of model classes (500+) in the Bladed NG input API. They are all accessible via the models module.

The root model is BladedAnalysis; a JSON file input to the calculation engine must have this model as the root object.

However the same capabilities are available for every model; each one can be read and written to JSON individually, as demonstrated below.

Load a full Bladed NG JSON analysis model from file

analysis = models.BladedAnalysis.from_file('/path/to/analysis.json')

This will perform some validation of the input to ensure the structure adheres to the input model schema.

Save a model to a JSON file

analysis.to_file('/path/to/file.json')

The JSON file can then be opened in VS Code, and will automatically receive validation, doc-string and auto-complete support against the Bladed NG JSON Schema.

Load a model from a JSON string

analysis = models.BladedAnalysis.from_json(json_str)

This will perform some validation of the input to ensure the structure adheres to the input model schema.

Render a model as a JSON string

json_str = analysis.to_json()

Create a new model object in code

Create a new instance of the root model, 'BladedAnalysis':

analysis = models.BladedAnalysis()

A model object can be created with an empty initialiser as shown above, or by specifying some or all of the child models as keyword arguments:

beam = models.LidarBeam(
    MountingPosition=models.LidarMountingPosition(
        X=1,
        Y=2,
        Z=3
    )
)

Modify a model object in code

If a model object is already loaded, properties can be modified as required:

analysis.SteadyCalculation.TipSpeedRatioRange.Minimum = 4.
analysis.SteadyCalculation.TipSpeedRatioRange.Maximum = 10.
analysis.SteadyCalculation.TipSpeedRatioRange.Interval = 0.1

Manipulate the turbine assembly

Access existing component definitions:

# Access a known existing component by it's key
blade: models.Blade = analysis.ComponentDefinitions['blade']

# Iterate over all component entries...
for key, component in analysis.ComponentDefinitions.items():
    print(f"Component key: {key}, Component type: {component.ComponentType}")

# Or just the keys
for key in analysis.ComponentDefinitions.keys():
    print(key)

# Or just the components
for component in analysis.ComponentDefinitions.values():
    print(component.ComponentType)

Access existing nodes in the Assembly tree using string and integer accessors:

blade_node = analysis.Turbine.Assembly['hub']['pitch-system-1'][0]
# or
blade_node = analysis.Turbine.Assembly['hub']['pitch-system-1']['blade-1']
# or
blade_nodes = [ps_node[0] for node_name, ps_node in analysis.Turbine.Assembly['hub'].items()]

Add new nodes and component definitions:

analysis.ComponentDefinitions['my-hub'] = models.IndependentPitchHub()
analysis.ComponentDefinitions['my-pitch-system'] = models.PitchSystem()
analysis.ComponentDefinitions['my-blade'] = models.Blade()

hub_node = models.AssemblyNode(
    ComponentReference = "#/ComponentDefinitions/my-hub"
)
for i in range(1,4):
    blade_node = models.AssemblyNode(
        ComponentReference = "#/ComponentDefinitions/my-blade"
    )
    ps_node = models.AssemblyNode(
        ComponentReference = "#/ComponentDefinitions/my-pitch-system"
    )
    ps_node[f'blade-{i}'] = blade_node
    hub_node[f'pitch-system-{i}'] = ps_node
analysis.Turbine.Assembly['hub'] = hub_node

Change a model to an alternative choice

Some model properties can be set to one of a number of different model types, to allow a choice between different options available in the calculation.

The property must simply be set to an object of one of the valid types. The valid types available are included in the doc strings, and the schema documentation available on the Bladed Next Gen website.

The example below is for dynamic stall. The detail of setting the specific properties on each model is omitted for brevity:

analysis.Aerodynamics.DynamicStall = models.OyeModel()

# or
analysis.Aerodynamics.DynamicStall = models.IAGModel()

# or
analysis.Aerodynamics.DynamicStall = models.CompressibleBeddoesLeishmanModel()

# or
analysis.Aerodynamics.DynamicStall = models.IncompressibleBeddoesLeishmanModel()

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