Force limited random vibration testing: the computation of the semi-empirical constant $$C^2$$ C 2 for a real test article and unknown supporting structure-Reference-Cited by-同舟云学术

Force limited random vibration testing: the computation of the semi-empirical constant $$C^2$$ C 2 for a real test article and unknown supporting structure

Published:2015-04-14 Issue:3 Volume:7 Page:359-373
ISSN:1868-2502
Container-title:CEAS Space Journal
language:en
Short-container-title:CEAS Space J

Author:

Wijker J. J.,Ellenbroek M. H. M.,Boer A. de

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1007/s12567-015-0086-0.pdf

Reference31 articles.

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3. Blevins, R.D.: Formulas for natural frequency and mode shape. Krieger Publishing Company (ISBN 0-89464-894-2) (1995)

4. Chang, K.Y.: Structural loads prediction in force-limited vibration testing. In Spacecraft & Lauch Vehicle Dynamic Environment Workshop, El Segundo, Calif., June 25–27 2002. The Aerospave Corporation (2002)

5. Coté, A., Sedaghati, R., Soucy, Y.: Force-limited vibration complex two-degree-of-system method. AIAA J. 42(6), 1208–1218 (2004)

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