Continuation of the near acoustic field of a jet to the far field. Part II: Experimental validation and noise source characteristics

16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)

Volumn , Issue , 2010, Pages

  Tam, Christopher K W ^a,c   Viswanathan, K ^b,d   Pastouchenko, Nikolai N ^a,d   Tam, Brian ^a,d  

^a FLORIDA STATE UNIVERSITY   (United States)

^b BOEING COMPANY   (United States)

^c Department of Mathematics and Florida   (United States)

^d Aeroacoustics and Fluid Mechanics ^*  (Uruguay)

Author keywords

[No Author keywords available]

Indexed keywords

APEX ANGLES; AXISYMMETRIC; AZIMUTHAL MODES; CONICAL SURFACES; CONTINUATION METHOD; CORRELATION FUNCTION; DEGREE OF RANDOMNESS; EQUIVALENT SOURCE; EXPERIMENTAL DATA; EXPERIMENTAL STUDIES; EXPERIMENTAL VALIDATIONS; FAR FIELD; FAR-FIELD NOISE; HIGH-SPEED JET; JET NOISE; MAXIMUM INTENSITIES; MICROPHONE ARRAYS; MODAL CHARACTERISTICS; NEAR FIELDS; NEAR-FIELD MEASUREMENT; NOISE SOURCE; NOZZLE EXITS; PROPAGATION SPEED; RADIATED NOISE; TIME PRESSURES; TWO-POINT; VALIDATION TEST;

ACOUSTIC FIELD MEASUREMENT; ACOUSTIC FIELDS; ACOUSTIC NOISE; ACOUSTIC NOISE MEASUREMENT; MICROPHONES;

AEROACOUSTICS;

EID: 78649576540     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (35)

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