Affiliation:
1. Fuels & Combustion Division, University of Dayton Research Institute, Dayton, OH 45469
2. Air Force Research Laboratory, Wright-Patterson AFB, Dayton, OH 45433
Abstract
Abstract
This work presents an open-source autonomous computational fluid dynamics (CFD) metamodeling environment (OpenACME) for small-scale combustor design optimization in a deterministic and continuous design space. OpenACME couples several object-oriented programing open-source codes for conjugate-heat transfer, steady-state, multiphase incompressible Reynolds averaged Navier-Stokes CFD-assisted engineering design metamodeling. There are fifteen design variables. Nonparametric rank regression (NPRR), global sensitivity analyses (GSA), and single-objective (SOO) optimization strategies are evaluated. The Euclidean distance (single-objective criterion) between a design point and the utopic point is based on the multi-objective criteria: combustion efficiency (η) maximization and pattern factor (PF), critical liner area factor (Acritical ), and total pressure loss (TPL) minimization. The SOO approach conducts Latin hypercube sampling (LHS) for reacting flow CFD for subsequent local constraint optimization by linear interpolation. The local optimization successfully improves the initial design condition. The SOO approach is useful for guiding the design and development of future gas turbine combustors. NPRR and GSA indicate that there are no leading-order design variables controlling η, pattern factor (PF), Acritical , and TPL. Therefore, interactions between design variables control these output metrics because the output design space is inherently nonsmooth and nonlinear. In summary, OpenACME is developed and demonstrated to be a viable tool for combustor design metamodeling and optimization studies.
Funder
Air Force Research Laboratory
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Reference35 articles.
1. Automated Design Optimization of a Small-Scale High-Swirl Cavity-Stabilized Combustor
2. Automated Design Optimization of a Small-Scale High-Swirl Cavity-Stabilized Combustor;ASME J. Eng. Gas Turbines Power,2018
3. Multiple-Objective Optimization of a Small-Scale Cavity-Stabilized Combustor,2019
4. Effect of Deterministic and Continuous Design Space Resolution on Multiple-Objective Combustor Optimization
5. LES-Verified RANS-Based Deterministic and Continuous Multiple-Objective Combustor Design Optimization
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