53rd AIAA Aerospace Sciences Meeting 2015
DOI: 10.2514/6.2015-1682
|View full text |Cite
|
Sign up to set email alerts
|

Integrating Subsystem Sizing into the More Electric Aircraft Conceptual Design Phase

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
5
0

Year Published

2018
2018
2021
2021

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 6 publications
(5 citation statements)
references
References 12 publications
0
5
0
Order By: Relevance
“…Chakraborty et al 3,5 developed an aircraft-specific conceptual design method, integrating sub-system architecture sizing with aircraft and propulsion sub-system sizing. It was further improved to cater for novel more electric architectures 4,15 . The method is aircraft specific while the computational workflows for sizing individual sub-systems as well as calculating system level performance are manually created.…”
Section: B State Of the Artmentioning
confidence: 99%
See 1 more Smart Citation
“…Chakraborty et al 3,5 developed an aircraft-specific conceptual design method, integrating sub-system architecture sizing with aircraft and propulsion sub-system sizing. It was further improved to cater for novel more electric architectures 4,15 . The method is aircraft specific while the computational workflows for sizing individual sub-systems as well as calculating system level performance are manually created.…”
Section: B State Of the Artmentioning
confidence: 99%
“…The default workflow satisfies the expression in Eq. (15). The independent inputs are as given in Table 6.…”
Section: Case-2: Under-determined System Of Modelsmentioning
confidence: 99%
“…The electro-thermal anti-icing system with CFRP composite has the advantages of simple and clean installation, convenient controllability, and efficient thermal response [ 5 ], which has attracted considerable research interest. This combination becomes highly applicable to the development of future aircraft that demands lightweight and eco-efficient systems and structures [ 6 ].…”
Section: Introductionmentioning
confidence: 99%
“…To prevent the aircraft wings and stabilizers from ice accretion, all commercial aircrafts are equipped with ice protection systems [2]. Generally, the thermal anti-icing system is the most widely used for large commercial aircraft and it also accounts for about 20% energy consumption of the aircraft engines [3][4][5]. Therefore, it is critical to optimize the thermal anti-icing system to achieve energy conservation, which can lighten the take-off weight and extend the flying range [6,7].…”
Section: Introductionmentioning
confidence: 99%