Algorithms and analyses for stochastic optimization for turbofan noise reduction using parallel reduced-order modeling
- Florida State University, Tallahassee, FL (United States); DOE/OSTI
- Florida State University, Tallahassee, FL (United States)
Simulation-based optimization of acoustic liner design in a turbofan engine nacelle for noise reduction purposes can dramatically reduce the cost and time needed for experimental designs. Because uncertainties are inevitable in the design process, a stochastic optimization algorithm is posed based on the conditional value-at-risk measure so that an ideal acoustic liner impedance is determined that is robust in the presence of uncertainties. A parallel reduced-order modeling framework is developed that dramatically improves the computational efficiency of the stochastic optimization solver for a realistic nacelle geometry. The reduced stochastic optimization solver takes less than 500 s to execute. Additionally, well-posedness and finite element error analyses of the state system and optimization problem are provided.
- Research Organization:
- Florida State University, Tallahassee, FL (United States)
- Sponsoring Organization:
- Air Force Office of Scientific Research (AFOSR); USDOE; USDOE Office of Science (SC)
- Grant/Contract Number:
- SC0010678
- OSTI ID:
- 1533650
- Journal Information:
- Computer Methods in Applied Mechanics and Engineering, Journal Name: Computer Methods in Applied Mechanics and Engineering Journal Issue: C Vol. 319; ISSN 0045-7825
- Publisher:
- ElsevierCopyright Statement
- Country of Publication:
- United States
- Language:
- English
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