Adaptive Finite Element in Time Method for Rotorcraft Analysis Using Element Size Control (AIAA 2016-1487)
AIAA/ASCE/AHS/ASC Structures, structural dynamics and materials (Conference)
2016-01-01
7 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Hybrid Finite Element Analysis of a Rotorcraft
SAE Technical Papers | 2013
|Hybrid Finite Element Analysis of a Rotorcraft
British Library Conference Proceedings | 2013
|Maneuvering Rotorcraft Simulations Using CREATE™ -AV Helios (AIAA 2016-1057)
British Library Conference Proceedings | 2016
|Micro-Scale Crack Propagation Using the eXtended Finite Element Method (AIAA 2016-0729)
British Library Conference Proceedings | 2016
|