Surrogate based design optimisation of composite aerofoil cross-section for helicopter vibration reduction

Title
Surrogate based design optimisation of composite aerofoil cross-section for helicopter vibration reduction
Authors
Keywords
-
Journal
AERONAUTICAL JOURNAL
Volume 116, Issue 1181, Pages 709-725
Publisher
Cambridge University Press (CUP)
Online
2016-02-05
DOI
10.1017/s0001924000007181

Ask authors/readers for more resources

Find Funding. Review Successful Grants.

Explore over 25,000 new funding opportunities and over 6,000,000 successful grants.

Explore

Publish scientific posters with Peeref

Peeref publishes scientific posters from all research disciplines. Our Diamond Open Access policy means free access to content and no publication fees for authors.

Learn More