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Finite element model updating of liquid rocket engine nozzle based on modal test results obtained from 3-D SLDV technique

  • Published:2017-10 Issue: Volume:69 Page:412-418
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Yan Song,Li Bin,Li Feng,Li Binchao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference19 articles.

1. Understanding critical dynamic loads for nozzle and nozzle extension design;Baker,2011

2. E.L. Blades, M. Baker, C.L. Pray, et al., Fluid–structure interaction simulations of rocket engine side loads, in: 2012 SIMULIA Customer Conference.

3. Finite Element Model Updating in Structural Dynamics;Friswell,1995

4. Finite element modelling and updating of a lively footbridge: the complete process;Ivanović;J. Sound Vib.,2007

5. Computational model updating and validation of aero-engine finite element models based on vibration test data;Boswald,2005

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