Boundary layer induced noise in aircraft, part II: The trimmed flat plate model

Journal of Sound and Vibration

Volumn 192, Issue 1, 1996, Pages 121-138

  Graham, W R ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE TRANSMISSION; AIRCRAFT; ATTENUATION; CABINS (AIRCRAFT); DAMPING; ENERGY ABSORPTION; HEAT LOSSES; MODELS; PLATES (STRUCTURAL COMPONENTS); RESONANCE; SOUND INSULATION; SURFACES;

ACOUSTIC EQUATIONS; BOUNDARY LAYER INDUCED NOISE; CABIN INTERIOR TREATMENT; SOUND RADIATION; TRIMMED FLAT PLATE MODEL; WAVENUMBER;

ACOUSTIC NOISE;

EID: 0030122620     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1996.0179     Document Type: Article

References (17)

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