2014
DOI: 10.1007/s11081-014-9273-7
|View full text |Cite
|
Sign up to set email alerts
|

A modified variable complexity modeling for efficient multidisciplinary aircraft conceptual design

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
13
0
1

Year Published

2015
2015
2024
2024

Publication Types

Select...
5
2

Relationship

0
7

Authors

Journals

citations
Cited by 28 publications
(14 citation statements)
references
References 29 publications
0
13
0
1
Order By: Relevance
“…On the downside, MDF is based on fixed-point iterations, and as a result, it requires a full analysis cycle for every one of the global evaluations which in turn can be a very computationally expensive process when timedemanding analyses or complex disciplinary couplings are considered [3,5]. A common application of MDF in aircraft design is the decomposition of coupled disciplines, and the most typical example of this is the concurrent evaluation of the mission performance (fuel requirements) and the estimation of the total weight [12,16,25,37,45,50,109]. Accordingly, further uses of the MDF architecture include the decoupling between performance and propulsion [12,18,51], aerodynamics and stability [12,61], and lastly, structures and loads which is a very common requirement when an accurate aeroelastic state must be determined [32,35,36,45,60,88,90,92,110].…”
Section: Decomposition Architecturesmentioning
confidence: 99%
See 1 more Smart Citation
“…On the downside, MDF is based on fixed-point iterations, and as a result, it requires a full analysis cycle for every one of the global evaluations which in turn can be a very computationally expensive process when timedemanding analyses or complex disciplinary couplings are considered [3,5]. A common application of MDF in aircraft design is the decomposition of coupled disciplines, and the most typical example of this is the concurrent evaluation of the mission performance (fuel requirements) and the estimation of the total weight [12,16,25,37,45,50,109]. Accordingly, further uses of the MDF architecture include the decoupling between performance and propulsion [12,18,51], aerodynamics and stability [12,61], and lastly, structures and loads which is a very common requirement when an accurate aeroelastic state must be determined [32,35,36,45,60,88,90,92,110].…”
Section: Decomposition Architecturesmentioning
confidence: 99%
“…A multifidelity scheme which has been frequently implemented in MDO frameworks for aircraft design and has often shown promising results is to include one more high-fidelity processes in order to calibrate or enhance the predictions of the low-fidelity tools. The development methodology which is followed in these cases is to use the simple models to initially narrow down the design space and then to engage a set of detailed analyses in order to obtain more reliable calculations over a smaller region [26,109]. The main advantages of this approach is that it firstly enables a quick exploration of the design tradeoffs at a complete discipline and aircraft level [46,114], while secondly, it allows the consideration of unconventional configurations and the use of advanced physics in areas where this is truly needed [27,32].…”
Section: Multifidelity Schemesmentioning
confidence: 99%
“…Besides a large number of studies of product design had been made on the PLM like the product concept design, the detailed design, the production and etc. [35][36][37][38][39], but there was no relevant research on the stage of customer requirement analysis.…”
Section: 2requirement Analysismentioning
confidence: 99%
“…Generally, type 1 and type 2 can be used in local VF modeling approaches, type 2 can also be used globally by adopting global metamodels to approximate the scaling function Cðx; aÞ, e.g., Kriging scaling [20][21][22], RBF scaling methods [23][24][25], etc. These two types of VF metamodeling have been successfully applied to the field of design optimization, and type 3 is based on a deeper understanding of a process being modeled, which can be useful but is problem dependent.…”
Section: Support Vector Regressionmentioning
confidence: 99%
“…The main shortcoming of these approaches is that they are only suitable for local optimization problems [17][18][19]. While in global VF modeling approaches, the scaling function is approximated using global metamodels, e.g., Kriging scaling methods [20][21][22], RBF scaling methods [23][24][25] and Bayesian-Gaussian scaling methods [19,[26][27][28]. Since global VF modeling approaches can mimic the behavior of the system on the entire domain and cope with multiple optimum problems sophisticatedly, there has been widespread concern about these approaches [12,29].…”
Section: Introductionmentioning
confidence: 99%