Transmission loss of a panel excited by turbulent boundary layer pressure field

Proceedings - National Conference on Noise Control Engineering

Volumn 1, Issue , 1996, Pages 205-210

  Mathur, Gopal P ^a   Chin, Cliff L ^a   Simpson, Myles A ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; ALUMINUM; BOUNDARY LAYERS; DIFFERENCE EQUATIONS; FINITE ELEMENT METHOD; FUSELAGES; MATHEMATICAL MODELS; MATRIX ALGEBRA; PRESSURE EFFECTS; STRUCTURAL PANELS; SUBSONIC AERODYNAMICS; TURBULENCE;

ACOUSTIC EXCITATION; MACH NUMBER; TRANSMISSION LOSS; TURBULENT BOUNDARY LAYER EXCITATION;

ACOUSTIC WAVE TRANSMISSION;

EID: 0030362592     PISSN: 07362935     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)