Enhanced vibration controllability by minor structural modifications
- 1 August 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 23 (8) , 1260-1266
- https://doi.org/10.2514/3.9075
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
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- Design for temperature and thermal buckling constraints employing a noneigenvalue formulationJournal of Spacecraft and Rockets, 1983
- Optimum actuator placement, gain, and number for a two-dimensional grillagePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Derivatives of eigenvalues and eigenvectorsAIAA Journal, 1970