Coupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure

A mathematical model and a computer code have been developed to fully couple the vibration of an aircraft fuselage panel to the surrounding flowfield, turbulent boundary layer and acoustic field.

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Bibliographische Detailangaben
Veröffentlicht in:	AIAA journal 1997-01, Vol.35 (1), p.58-66
1. Verfasser:	Frendi, Abdelkader
Format:	Artikel
Sprache:	eng
Schlagworte:	Acoustics Aerodynamics Aircraft Exact sciences and technology Fundamental areas of phenomenology (including applications) Mathematical models Physics Structural acoustics and vibration Turbulence
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	A mathematical model and a computer code have been developed to fully couple the vibration of an aircraft fuselage panel to the surrounding flowfield, turbulent boundary layer and acoustic field.
ISSN:	0001-1452 1533-385X
DOI:	10.2514/2.87