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Application of High-order Panel Method in Static Aeroelastic Analysis of Aircraft

✍ Scribed by Yaokun Wang; Zhiqiang Wan; Chao Yang

Book ID
119356308
Publisher
Elsevier
Year
2012
Tongue
English
Weight
447 KB
Volume
31
Category
Article
ISSN
1877-7058

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The classical and the high-order computational models of unidirectional sandwich panels with incompressible and compressible cores are presented. The significant theoretical and practical differences are discussed and elaborated through some numerical examples of typical sandwich panels. The classic