Effect of Longitudinal Stringers on Sound Transmission into a Thin Cylindrical Shell
- 1 December 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 15 (12) , 816-821
- https://doi.org/10.2514/3.58454
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- On sound transmission into a heavily-damped cylinderJournal of Sound and Vibration, 1978
- Effect of Stiffening on Sound Transmission into a Cylindrical Shell in FlightAIAA Journal, 1977
- On sound transmission into a thin cylindrical shell under “flight conditions”Journal of Sound and Vibration, 1976
- Free Vibrations of Longitudinally Stiffened Cylindrical ShellsJournal of Applied Mechanics, 1974
- Vibrations of axially loaded stiffened cylindrical shellsJournal of Sound and Vibration, 1974
- Vibration of simply supported cylindrical shells with longitudinal stiffenersJournal of Sound and Vibration, 1972
- An analysis of free vibration of orthogonally stiffened cylindrical shells with stiffeners treated as discrete elements.AIAA Journal, 1968
- Sound Transmission through Thin Cylindrical ShellsThe Journal of the Acoustical Society of America, 1957