Control of gas turbine stator blade vibrations by means of enamel coatings
- 1 April 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 12 (4) , 226-230
- https://doi.org/10.2514/3.44436
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Temperature-frequency dependence of dynamic properties of damping materialsJournal of Sound and Vibration, 1974