Integration of acoustics and mechanics in a stiffened shell fuselage. Part III

Applied Composite Materials

Volumn 12, Issue 1, 2005, Pages 21-35

  Krakers, L A ^a   Van Tooren, M J L ^a   Zaal, K ^a   Vermeeren, C A J R ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

Multi disciplinary design; Sound transmission loss; Stiffened fuselage structure

Indexed keywords

ALUMINUM; BUCKLING; CARBON FIBER REINFORCED PLASTICS; INTEGRATION; SOUND INSULATION; STIFFNESS; STRESS ANALYSIS; STRUCTURAL ANALYSIS; THICKNESS MEASUREMENT;

MULTI-DISCIPLINARY DESIGN; OPTIMAL INTEGRATION; SOUND TRANSMISSION LOSS; STIFFENED FUSELAGE STRUCTURES; STRUCTURAL PARAMETERS;

FUSELAGES;

EID: 14644435727     PISSN: 0929189X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s10443-004-4217-6     Document Type: Conference Paper

References (4)

1. van Tooren, M. J. L., Sandwich Fuselage Design, 010 publishers, Rotterdam, 1998.
2. Fahy, F., Sound and Structural Vibration, Radiation, Transmission and Response, Academic Press, London, 1989.
3. von Venzke, G., Dämmig, P. and Fischer, H. W., 'Der Einfluß von Versteifungen auf die Schallabstrahlung und Schalldämmung von Metallwänden', Acustica 29(1), 1973, 29-40.
4. Beranek, L. L., Noise and Vibration Control, Institute of Noise Control Engineering, Washington, DC, 1988.