emissions

class description

class emissions.Emissions(**kwargs)[source]

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Compute emission characteristics of engine on the trajectory.

The Emissions component requires the following inputs:

  • inputs['Tti_c_star']: combustor inlet temperature (re. T_0) [-]

  • inputs['Pti_c_star']: combustor inlet pressure (re. p_0) [-]

  • inputs['W_f']: engine fuel flow [kg/s]

  • inputs['p_0']: ambient pressure [Pa]

  • inputs['T_0']: ambient temperature [K]

  • inputs['t_s']: source time [s]

The Emissions component computes the following outputs:

  • outputs['EINOx']: NOx emission index [g/kg fuel]

  • outputs['m_NOx']: Total mass of NOx emitted on the trajectory [kg]

compute(inputs: openmdao.vectors.default_vector.DefaultVector, outputs: openmdao.vectors.default_vector.DefaultVector)[source]

Compute outputs given inputs. The model is assumed to be in an unscaled state.

Parameters
  • inputs (Vector) – Unscaled, dimensional input variables read via inputs[key].

  • outputs (Vector) – Unscaled, dimensional output variables read via outputs[key].

  • discrete_inputs (dict or None) – If not None, dict containing discrete input values.

  • discrete_outputs (dict or None) – If not None, dict containing discrete output values.

compute_partials(inputs, partials)[source]

Compute sub-jacobian parts. The model is assumed to be in an unscaled state.

Parameters
  • inputs (Vector) – Unscaled, dimensional input variables read via inputs[key].

  • partials (Jacobian) – Sub-jac components written to partials[output_name, input_name]..

  • discrete_inputs (dict or None) – If not None, dict containing discrete input values.

initialize()[source]

Perform any one-time initialization run at instantiation.

setup()[source]

Declare inputs and outputs.

Available attributes:

name pathname comm options

theory

The combustor emissions along the trajectory are computed using the \(P_3-T_3\) method.