Skip to main content
Disciplines
Automotive Business IT + Informatics Construction + Real Estate Electrical Engineering + Electronics Energy + Sustainability Insurance + Risk Finance + Banking Management + Leadership Marketing + Sales Mechanical Engineering + Materials
Events
DE
EN
Books
Journals
Topic Page
Marketing
Start single access now
Access for companies
EXTENDED SEARCH
Log in
Top
Published in:
A Study of Hybrid Airfoil Design Method Read chapter Read first chapter

2019 | OriginalPaper | Chapter

Multi-disciplinary Optimization of Large Civil Aircraft Using a Coupled Aero-Structural Adjoint Approach

Authors : Jiangtao Huang, Jing Yu, Zhenghong Gao, Zhu Zhou, Biaosong Chen

Published in: The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018)

Publisher: Springer Singapore

Log in

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

The coupled aero-structural adjoint-based approach for large civil aircraft multi-disciplinary optimization is studied in this paper. Firstly, computational techniques are introduced. Then the coupled aero-structural adjoint system (CASA) is developed and constructed, solving the structural adjoint equations derived from the structural static equations, with the help of the parallel flow adjoint code PADJ3D and lagged coupled adjoint method. Afterwards, the multi-disciplinary optimization model for the large civil aircraft is established, while the sequential quadratic programming algorithm is used for optimization, freeform deformation method is employed for geometric parameterization and parallel RBF-TFI grid reconstruction technology is used for mesh perturbation. On accounting of the coupled aerodynamic and structural disciplines, the multi-disciplinary optimization for large civil aircraft wing is carried out based on the developed CASA system. The simulation results demonstrate the effectiveness of the CASA system. Under the stress constraints, the aerodynamic drag and the structural weight can be effectively optimized.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

inform now

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

inform now
previous chapter Low Boom Supersonic Aircraft Configuration Optimization Using Inverse Design Method
next chapter Efficiency Estimation of Formation Flight Types
Literature
1.
Joaquim RRA, Martins A (2002) Coupled-adjoint method for high-fidelity. aero-structural optimization. The department of aeronautics and astronautics and the committee of stanford university 2002
2.
Mader CA, Kenway GKW, Martins JRRA (2008) Towards high-fidelity aerostructural optimization using a coupled adjoint approach. In: 12th AIAA/ISSMO multidisciplinary analysis and optimization conference, 10–12 September 2008, Victoria, British Columbia, Canada
3.
Kenway GKW, Kennedy GJ, Martins JRRA (2014) Scalable parallel approach for high-fidelity steady-state aeroelastic analysis and adjoint derivative computations. AIAA J 52(5):935–951CrossRef
4.
Martins JRRA, Hwang JT (2013) Review and unification of methods for computing derivatives of multidisciplinary computational models. AIAA J 51(11):2582–2599CrossRef
5.
Kenway GKW, Martins JRRA (2014) Multipoint high-fidelity aerostructural optimization of a transport aircraft configuration. J Aircr 51(1):144–160CrossRef
6.
Kennedy G, Martins J (2010) Parallel solution methods for aerostructural analysis and design optimization. In: 13th AIAA/ISSMO multidisciplinary analysis optimization conference, p 9308
7.
Martins JRRA, Alonso JJ, Reuther JJ (2004) High-fidelity aerostructural design optimization of a supersonic business jet. J Aircr 41(3):523–530CrossRef
8.
Leoviriyakit K, Jameson A (2002) Case studies in aero-structural wing planform and section optimization. In: AIAA, p 5372
9.
Abu-Zurayk M, Brezillon J (2011) Shape optimization using the aerostructural coupled adjoint approach for viscous flows. In: Evolutionary and deterministic methods for design, optimization and control.© CIRA, Capua, Italy
10.
Ghazlane I, Carrier G, Dumont A (2012) Aerostructural adjoint method for flexible wing optimization. In: AIAA, p 1924
11.
Marcelet M, Peter J, Carrier G (2008) Sensitivity analysis of a strongly coupled aero-structural system using direct and adjoint methods. In: AIAA, p 5863
12.
Gang L, Zhongyun X, Jiantao W, Fan L (2015) Numerical simulation of missile air-launching process under rail slideway constraints. ACTA Aerodynamica Sinica 33(02):192–197
13.
Spekreijse SP, Boerstoel JW (1998) An algorithm to check the topological validity of multi-block domain decompositions. In: Proceedings 6th international conference on numerical grid generation in computational field simulations, NLR-TP-98, Greenwich, p 198
14.
Hua QIN, Yanzi XU (2011) Improving SVM’s learning efficiency by using matrix LDLT parallel decomposition. Comput Eng Appl 47(12):200–212
15.
Huang JT, Liu G, Zhou Z et al (2017) Investigation of gradient computation based on discrete adjoint method. Acta Aerodynamica Sinica 35(4):554–562
16.
Allen CB, Rendall TCS (2007) Unified approach to CFD-CSD interpolation and mesh motion using radial basis functions. In: AIAA, p. 3804
17.
Zhang H, Chen B, Li Y et al (2011) Advancement of SiPESC for development of integrated CAE software systems. Comput. Aided Eng. 20(2):39–49
18.
Huang J, Zhou Z, Liu G, Gao Z, Huang Y, Wang Y (2018) Numerical study of aero-structural multidisciplinary lagged coupled adjoint system for aircraft. ACTA Aeronauticaet Astronautica Sinica 39(5):121731
19.
Wang YT, Zhang SJ, Meng DH (2013) Numerical simulation and study for DPW4 wing/body/tail. ACTA Aerodynamic Sinica 31(6):739–744
20.
Vassberg JC, Dehaan MA, Rivers SM, et al (2008) Development of a common research model for applied CFD validation studies. In: AIAA, p 6919
Metadata
Title
Multi-disciplinary Optimization of Large Civil Aircraft Using a Coupled Aero-Structural Adjoint Approach
Authors
Jiangtao Huang
Jing Yu
Zhenghong Gao
Zhu Zhou
Biaosong Chen
Copyright Year
2019
Publisher
Springer Singapore
Book
The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018)

Print ISBN: 978-981-13-3304-0

Electronic ISBN: 978-981-13-3305-7

Copyright Year: 2019

DOI
https://doi.org/10.1007/978-981-13-3305-7_83

Premium Partner

    Image Credits