Update search
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
NARROW
Format
Journal
Type
Issue Section
Date
Availability
1-3 of 3
Keywords: Sizing
Close
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
Sort by
Journal Articles
Automated model generation and sizing of aircraft structures
Available to Purchase
Aircraft Engineering and Aerospace Technology: An International Journal (2016) 88 (2): 268–276.
Published: 07 March 2016
... for the aircraft preliminary design process. It is based on the common parametric aircraft configuration schema (CPACS), which is an abstract aircraft namespace. DELiS facilitates interfaces to several commercial and non-commercial finite element solvers and sizing tools. Findings The key principles...
Journal Articles
Automated sizing of a composite wing for the usage within a multidisciplinary design process
Available to Purchase
Aircraft Engineering and Aerospace Technology: An International Journal (2016) 88 (2): 303–310.
Published: 07 March 2016
... is capable of dealing with different design concepts and novel materials properly. The functionality of the module is also demonstrated. Design/methodology/approach For fast sizing and optimization, linear static finite element (FE) models are used to obtain inner loads of the structural components...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2000) 72 (3)
Published: 01 June 2000
... © MCB UP Limited 2000 --> Aerospace Composite Technologies Wind tunnels Malvern Instruments Particles Sizing Keywords Aerospace Composite Technologies, Wind tunnels, Malvern Instruments,Particles, Sizing A new state-of-the-art icing wind tunnel at Aerospace Composite...
