Two‐dimensional analytical model of twin jet shielding

• 1 April 1981
• journal article
• Published by Acoustical Society of America (ASA) in The Journal of the Acoustical Society of America
• Vol. 69  (4) , 904-908
• https://doi.org/10.1121/1.385611

Abstract

Keywords

• HEAT FLOW
• SHIELDING
• MATHEMATICAL MODEL
• SOUND PRESSURE
• NOISE REDUCTION
• ACOUSTIC ATTENUATION
• FREQUENCY RESPONSE
• MATHEMATICAL MODELS
• WAVE EQUATION