Stress and deflection of honeycomb panels loaded by spatially uniform white noise.
- 1 August 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (8) , 1503-1510
- https://doi.org/10.2514/3.4796
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- The Random Vibration Response of a System Having Many Degrees of FreedomAeronautical Quarterly, 1966
- Forced Vibrations of Cylindrical Sandwich ShellsJournal of the Aerospace Sciences, 1962
- Simplified Vibration Analysis of Elastic Sandwich PlatesJournal of the Aerospace Sciences, 1960
- On the Fatigue Failure of Structures due to Vibrations Excited by Random Pressure FieldsThe Journal of the Acoustical Society of America, 1958
- On transverse vibrations of thin, shallow elastic shellsQuarterly of Applied Mathematics, 1955