Multidisciplinary Design Optimization Based on Parameterized Free-Form Deformation for Single Turbine-Reference-Cited by-同舟云学术

Multidisciplinary Design Optimization Based on Parameterized Free-Form Deformation for Single Turbine

Published:2019-05 Issue:5 Volume:57 Page:2075-2087
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Li Lei¹,Yuan Tianyu¹,Li Yuan¹,Yang Weizhu¹,Kang Jialei¹

Affiliation:

1. Northwestern Polytechnical University, 710129 Xi’an, People’s Republic of China

Funder

Natural Science Basic Research Plan in Shaanxi Province of China

Aviation Power Foundation

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057819

Reference36 articles.

1. Sobieszczanski-SobieskiJ. “A Linear Decomposition Method for Large Optimization Problems. Blueprint for Development,” NASA TM-83248, 1982.

2. Multidisciplinary Design Optimization: An Emerging New Engineering Discipline

3. Development of a Multidisciplinary Design Optimization Framework Applied on UAV Design by Considering Models for Mission, Surveillance, and Stealth Performance

4. MartinsJ. R. R. A.KenwayG. K. W.BurdetteD.JonssonE.KennedyG. J. “High-Fidelity Multidisciplinary Design Optimization of Aircraft Configurations,” NASA CR-2017-219647, 2017.

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