Nonintrusive reduced order model for parametric solutions of inertia relief problems

Author:

Cavaliere Fabiola123ORCID,Zlotnik Sergio12ORCID,Sevilla Ruben3ORCID,Larráyoz Xabier4,Díez Pedro12ORCID

Affiliation:

1. Laboratori de Càcul Numeric (LaCàN), E.T.S. de Ingenieros de Caminos, Canales y Puertos Universitat Politecnica de Catalunya Barcelona Spain

2. International Centre for Numerical Methods in Engineering CIMNE Barcelona Spain

3. Zienkiewicz Centre for Computational Engineering College of Engineering Swansea University Swansea Wales UK

4. Centro Técnico de SEAT S.A Martorell Spain

Funder

Engineering and Physical Sciences Research Council

Generalitat de Catalunya

H2020 Marie Skłodowska-Curie Actions

Ministerio de Economía y Competitividad

Publisher

Wiley

Subject

Applied Mathematics,General Engineering,Numerical Analysis

Reference45 articles.

1. Mechanical Vibrations in Spacecraft Design

2. The use of inertia relief to estimate impact loads;Nelson MF;SAE Transactions,1977

3. BarnettAR WidrickTW LudwiczakDR. Closed‐form static analysis with inertia relief and displacement‐dependent loads using a MSC/NASTRAN DMAP Alter;1995.

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