Assessment of 3D codes for predicting liner attenuation in flow ducts

14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)

Volumn , Issue , 2008, Pages

  Watson, W R ^a,b   Nark, D M ^a,b   Jones, M G ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Research and Technology Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; BOUNDARY CONDITIONS; CLOCKS; DUCTS; FORECASTING; NASA; NUMERICAL METHODS; POLYNOMIALS; SUPERCOMPUTERS; TIME DOMAIN ANALYSIS;

APPROXIMATE RESULTS; CUBIC HERMITE; FINITE ELEMENT CODES; GOVERNING DIFFERENTIAL EQUATIONS; LINER ATTENUATION; LINER IMPEDANCE; PARABOLIC APPROXIMATION; THREE DIMENSIONAL CODE;

CODES (SYMBOLS);

EID: 78249243423     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-2828     Document Type: Conference Paper

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