Aerodynamic Shape Optimization of a Gas Turbine Engine Air-Delivery Duct-Reference-Cited by-同舟云学术

Aerodynamic Shape Optimization of a Gas Turbine Engine Air-Delivery Duct

Published:2020-07 Issue:4 Volume:33 Page:04020042
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Marchlewski Krzysztof¹^ORCID,Łaniewski-Wołłk Łukasz²^ORCID,Kubacki Sławomir³

Affiliation:

1. Warsaw Univ. of Technology, Faculty of Power and Aeronautical Engineering, Institute of Aeronautics and Applied Mechanics, Nowowiejska 24, 00-665 Warsaw, Poland (corresponding author). ORCID: .

2. Warsaw Univ. of Technology, Faculty of Power and Aeronautical Engineering, Institute of Aeronautics and Applied Mechanics, Nowowiejska 24, 00-665 Warsaw, Poland. ORCID: .

3. Warsaw Univ. of Technology, Faculty of Power and Aeronautical Engineering, Institute of Aeronautics and Applied Mechanics, Nowowiejska 24, 00-665 Warsaw, Poland.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001157

Reference44 articles.

1. Node-Based Adjoint Surface Optimization of U-Bend Duct for Pressure Loss Reduction

2. Automated Design Optimization of a Three-Dimensional Subsonic Diffuser

3. Efficient global optimization for S-duct diffuser shape design;Bae H.;J. Aerosp. Eng.,2012

4. Bradstreet L. 2011. “The hypervolume indicator for multi-objective optimisation: Calculation and use.” Ph.D. thesis Univ. of Western Australia. https://research-repository.uwa.edu.au/en/publications/the-hypervolume-indicator-for-multi-objective-optimisation-calcul.

5. Carnell R. 2016. “LHS: Latin hypercube samples.” R package version 0.14. Accessed April 30 2020. https://CRAN.R-project.org/package=lhs.

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