Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model

Takayasu Kumano; Shinkyu Jeong; Shigeru Obayashi; Yasushi Ito; Keita Hatanaka; Hiroyuki Morino

doi:10.2514/6.2006-932

Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model

Takayasu Kumano, Shinkyu Jeong, Shigeru Obayashi, Yasushi Ito, Keita Hatanaka, Hiroyuki Morino

Creative Flow Research Division

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

38 Citations (Scopus)

Abstract

In this paper, a practical Multidisciplinary Design Optimization (MDO) system for an aircraft design is developed. The MDO system is based on the integration of computational fluid dynamics (CFD) codes and the NASTRAN based aeroelastic-structural interface code. Kriging model is employed to save the computational time of objective function evaluation in Multi-Objective Genetic Algorithm (MOGA). As a result of optimization, several nondominated solutions, indicating the trade-off among the drag, the structural weight, the drag divergence and the pitching moment, have been found.

Original language	English
Title of host publication	Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
Publisher	American Institute of Aeronautics and Astronautics Inc.
Pages	11158-11170
Number of pages	13
ISBN (Print)	1563478072, 9781563478079
DOIs	https://doi.org/10.2514/6.2006-932
Publication status	Published - 2006
Event	44th AIAA Aerospace Sciences Meeting 2006 - Reno, NV, United States Duration: 2006 Jan 9 → 2006 Jan 12

Publication series

Name	Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
Volume	15

Other

Other	44th AIAA Aerospace Sciences Meeting 2006
Country/Territory	United States
City	Reno, NV
Period	06/1/9 → 06/1/12

ASJC Scopus subject areas

Space and Planetary Science
Aerospace Engineering

Access to Document

10.2514/6.2006-932

Cite this

Kumano, T., Jeong, S., Obayashi, S., Ito, Y., Hatanaka, K., & Morino, H. (2006). Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model. In Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting (pp. 11158-11170). (Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting; Vol. 15). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2006-932

Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model. / Kumano, Takayasu; Jeong, Shinkyu; Obayashi, Shigeru et al.

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., 2006. p. 11158-11170 (Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting; Vol. 15).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Kumano, T, Jeong, S, Obayashi, S, Ito, Y, Hatanaka, K & Morino, H 2006, Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model. in Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting, vol. 15, American Institute of Aeronautics and Astronautics Inc., pp. 11158-11170, 44th AIAA Aerospace Sciences Meeting 2006, Reno, NV, United States, 06/1/9. https://doi.org/10.2514/6.2006-932

Kumano T, Jeong S, Obayashi S, Ito Y, Hatanaka K, Morino H. Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model. In Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc. 2006. p. 11158-11170. (Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting). doi: 10.2514/6.2006-932

Kumano, Takayasu ; Jeong, Shinkyu ; Obayashi, Shigeru et al. / Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model. Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., 2006. pp. 11158-11170 (Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting).

@inproceedings{bb4fddb6c4fe495e9b0f39675080791b,

title = "Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model",

abstract = "In this paper, a practical Multidisciplinary Design Optimization (MDO) system for an aircraft design is developed. The MDO system is based on the integration of computational fluid dynamics (CFD) codes and the NASTRAN based aeroelastic-structural interface code. Kriging model is employed to save the computational time of objective function evaluation in Multi-Objective Genetic Algorithm (MOGA). As a result of optimization, several nondominated solutions, indicating the trade-off among the drag, the structural weight, the drag divergence and the pitching moment, have been found.",

author = "Takayasu Kumano and Shinkyu Jeong and Shigeru Obayashi and Yasushi Ito and Keita Hatanaka and Hiroyuki Morino",

year = "2006",

doi = "10.2514/6.2006-932",

language = "English",

isbn = "1563478072",

series = "Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting",

publisher = "American Institute of Aeronautics and Astronautics Inc.",

pages = "11158--11170",

booktitle = "Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting",

note = "44th AIAA Aerospace Sciences Meeting 2006 ; Conference date: 09-01-2006 Through 12-01-2006",

}

TY - GEN

T1 - Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model

AU - Kumano, Takayasu

AU - Jeong, Shinkyu

AU - Obayashi, Shigeru

AU - Ito, Yasushi

AU - Hatanaka, Keita

AU - Morino, Hiroyuki

PY - 2006

Y1 - 2006

N2 - In this paper, a practical Multidisciplinary Design Optimization (MDO) system for an aircraft design is developed. The MDO system is based on the integration of computational fluid dynamics (CFD) codes and the NASTRAN based aeroelastic-structural interface code. Kriging model is employed to save the computational time of objective function evaluation in Multi-Objective Genetic Algorithm (MOGA). As a result of optimization, several nondominated solutions, indicating the trade-off among the drag, the structural weight, the drag divergence and the pitching moment, have been found.

AB - In this paper, a practical Multidisciplinary Design Optimization (MDO) system for an aircraft design is developed. The MDO system is based on the integration of computational fluid dynamics (CFD) codes and the NASTRAN based aeroelastic-structural interface code. Kriging model is employed to save the computational time of objective function evaluation in Multi-Objective Genetic Algorithm (MOGA). As a result of optimization, several nondominated solutions, indicating the trade-off among the drag, the structural weight, the drag divergence and the pitching moment, have been found.

UR - http://www.scopus.com/inward/record.url?scp=34250804357&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=34250804357&partnerID=8YFLogxK

U2 - 10.2514/6.2006-932

DO - 10.2514/6.2006-932

M3 - Conference contribution

AN - SCOPUS:34250804357

SN - 1563478072

SN - 9781563478079

T3 - Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

SP - 11158

EP - 11170

BT - Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

PB - American Institute of Aeronautics and Astronautics Inc.

T2 - 44th AIAA Aerospace Sciences Meeting 2006

Y2 - 9 January 2006 through 12 January 2006

ER -

Multidisciplinary design optimization of wing shape for a small jet aircraft using kriging model

Abstract

Publication series

Other

ASJC Scopus subject areas

Access to Document

Other files and links

Fingerprint

Cite this