[PDF][PDF] A robust and reliability-based optimization framework for conceptual aircraft wing design

RM Paiva - 2010 - dspace.library.uvic.ca
A robustness and reliability based multidisciplinary analysis and optimization framework for
aircraft design is presented. Robust design optimization and Reliability Based Design …

Robust and reliability-based design optimization framework for wing design

RM Paiva, C Crawford, A Suleman - AIAA journal, 2014 - arc.aiaa.org
This paper outlines an architecture for simultaneous analysis, robustness, and reliability
calculations in aircraft wing design optimization. Robust design optimization and reliability …

Robust optimization of a wing under structural and material uncertainties

K Boopathy, MP Rumpfkeil, RM Kolonay - 17th AIAA Non-Deterministic …, 2015 - arc.aiaa.org
This paper demonstrates structural sizing optimizations of a fighter wing configuration in the
presence of uncertainties in structural parameters and material properties. The design …

Aircraft multidisciplinary design optimization under both model and design variables uncertainty

L Jaeger, C Gogu, S Segonds, C Bes - Journal of Aircraft, 2013 - arc.aiaa.org
Low-fidelity analytical models are often used at the conceptual aircraft design stage.
Because of uncertainties on these models and their corresponding input variables …

Multidisciplinary design optimization of aircraft wing using commercial software integration

A Benaouali, S Kachel - Aerospace Science and Technology, 2019 - Elsevier
In this paper, a fully automated framework dedicated to the high-fidelity multidisciplinary
design optimization of aircraft wing is developed. This design framework integrates a set of …

Multidisciplinary optimization of wing structure using parametric models

K Amadori, T Melin, P Krus - … Meeting including the New Horizons Forum …, 2013 - arc.aiaa.org
ONCPTUAL design studies represent the basis for product development, and are decisive
for defining partnerships and positioning in global supply chains, identifying technical needs …

Aircraft wing box optimization considering uncertainty in surrogate models

D Neufeld, K Behdinan, J Chung - Structural and Multidisciplinary …, 2010 - Springer
Aerospace design often involves computationally expensive physics based analysis
methods such as Computational Fluid Dynamics (CFD) or the Finite Element Method (FEM) …

[图书][B] Multidisciplinary design optimization of aircraft wing structures with aeroelastic and aeroservoelastic constraints

SY Jung - 1999 - search.proquest.com
Abstract Design procedures for aircraft wing structures with control surfaces are presented
using multidisciplinary design optimization. Several disciplines such as stress analysis …

[PDF][PDF] Multidisciplinary design and optimization framework for aircraft box structures

R Van Dijk, X Zhao, H Wang… - 3rd Aircraft Structural …, 2012 - researchgate.net
Competitive aircraft box structures are a perfect compromise between weight and price. The
conceptual design process of these structures is a typical Multidisciplinary Design and …

A Framework for Aircraft Conceptual Design and Multidisciplinary Optimization

S Hosseini, MA Vaziry-Zanjany, HR Ovesy - Aerospace, 2024 - mdpi.com
In this research, the architecture and the functionalities of the LAMBDA (Laboratory of
Aircraft Multidisciplinary Knowledge-Based Design and Analysis) framework for the design …