Design criterion of panel structure excited by turbulent boundary layer.
- 1 July 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 5 (4) , 321-328
- https://doi.org/10.2514/3.43946
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
- THE RESPONSE OF SIMPLE PANELS TO TURBULENT BOUNDARY LAYER EXCITATIONPublished by Defense Technical Information Center (DTIC) ,1967
- Use of turbulent model to calculate the vibration and radiation responses of a panel, with practical suggestions for reducing sound levelJournal of Sound and Vibration, 1967
- Transduction of Boundary-Layer Noise by a Rectangular PanelThe Journal of the Acoustical Society of America, 1966
- Response of a Flexible Panel to Turbulent Flow: Running-Wave versus Modal-Density AnalysisThe Journal of the Acoustical Society of America, 1966
- Turbulence Measurements Relevant to Jet NoiseThe Journal of the Acoustical Society of America, 1966
- Effect of pressurization on airplane fuselage drag.Journal of Aircraft, 1965
- Flow Excitation of Cylindrical Shells and Associated Coincidence EffectsThe Journal of the Acoustical Society of America, 1964
- Response of Bars and Plates to Boundary-Layer TurbulenceJournal of the Aerospace Sciences, 1962
- On the Approximation to the “Infinite” Solution by the Method of Normal Modes for Random VibrationsThe Journal of the Acoustical Society of America, 1958
- Noise Transmission from Boundary Layer Pressure FluctuationsThe Journal of the Acoustical Society of America, 1957