Output details
12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering
Cranfield University
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Output 0 of 0 in the submission
Article title
Novel Uncertainty Propagation Method for Robust Aerodynamic Design
Type
D - Journal article
Title of journal
AIAA Journal
Article number
-
Volume number
49
Issue number
3
First page of article
530
ISSN of journal
0001-1452
Year of publication
2011
URL
-
Number of additional authors
2
Additional information
Initial research results from an EC 6th FP, Integrated Project, enabling robust design, were carried forward into the €50M CRESCENDO Integrated Project, under EC FP7, grant agreement number 234344 (www.crescendo-fp7.eu, Philippe.Homsi@airbus.com). The method, which allows a more efficient computation of uncertainty, also led to a NASA-funded research project (http://nasa.orau.org/postdoc/about-fellows/fellows-2011.htm) on a probabilistic approach to the design and optimisation of Boundary Layer Ingesting Inlets for novel aircraft configurations.
Interdisciplinary
-
Cross-referral requested
-
Research group
A - Aerospace Engineering
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
