NASA NTRS · 20170002541
Optimization of Turbine Engine Cycle Analysis with Analytic Derivatives
Abstract
A new engine cycle analysis tool, called Pycycle, was recently built using the OpenMDAO framework. This tool uses equilibrium chemistry based thermodynamics, and provides analytic derivatives. This allows for stable and efficient use of gradient-based optimization and sensitivity analysis methods on engine cycle models, without requiring the use of finite difference derivative approximation methods. To demonstrate this, a gradient-based design optimization was performed on a multi-point turbofan engine model. Results demonstrate very favorable performance compared to an optimization of an identical model using finite-difference approximated derivatives.
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Hearn, Tristan, Hendricks, Eric, Chin, Jeffrey, Gray, Justin, Moore, Kenneth T.. 2016-06-16. Optimization of Turbine Engine Cycle Analysis with Analytic Derivatives. https://ntrs.nasa.gov/citations/20170002541
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