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NASA NTRS · 20170000232

Optimization of Turbine Engine Cycle Analysis with Analytic Derivatives

Abstract

A new engine cycle analysis tool, called Pycycle, was built using the OpenMDAO framework. Pycycle provides analytic derivatives allowing for an efficient use of gradient-based optimization 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 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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BibTeXRIS

Hearn, Tristan, Hendricks, Eric, Chin, Jeffrey, Gray, Justin, Moore, Kenneth T.. 2016-06-13. Optimization of Turbine Engine Cycle Analysis with Analytic Derivatives. https://ntrs.nasa.gov/citations/20170000232

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