A Novel Method to Correlate a Rocket Launcher Finite Element Model Using Experimental Modal Test Measurements and Identification Algorithms-Reference-Cited by-同舟云学术

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A Novel Method to Correlate a Rocket Launcher Finite Element Model Using Experimental Modal Test Measurements and Identification Algorithms

Published:2016 Issue: Volume: Page:153-166
ISSN:2191-5644
Container-title:Shock & Vibration, Aircraft/Aerospace, Energy Harvesting, Acoustics & Optics, Volume 9
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Author:

Couch Ronald N.,Radcliffe Eliott J.,Caldwell Rickey A.

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-319-30087-0_14

Reference12 articles.

1. Mottershead, J.E., Friswell, M.I.: Model updating in structural dynamics: a survey. J. Sound Vib. 167(2), 347–375 (1993)

2. Zarate, B.A., Caicedo, J.M.: Finite element model updating: multiple alternatives. Eng. Struct. 30, 3724–3730 (2008)

3. Juang, J., Pappa, R.S.: An eigensystem realization algorithm for modal parameter identification and model reduction. AIAA J. Guid. Control Dyn. 8(5), 620–627 (1985)

4. Maia, S.: Theoretical and Experimental Modal Analysis Research Studies Press LTD (1997)

5. Pappa, R.S., Elliott, K.B., Schenk, A.: Consistent-mode indicator for the eigensystem realization algorithm. J. Guid. Control Dyn. 16(5), 852–858 (1993)

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1. Weight and configuration optimization of the launcher pod using finite element analysis;The Journal of Defense Modeling and Simulation: Applications, Methodology, Technology;2021-12-29

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