Far-field noise control in supersonic jets from conical and contoured nozzles

Journal of Engineering for Gas Turbines and Power

Volumn 133, Issue 8, 2011, Pages

  Kim, Jin Hwa ^a   Kearney Fischer, Martin ^a   Samimy, Mo ^a   Gogineni, Sivaram ^b  

^a OHIO STATE UNIVERSITY   (United States)

^b 5100 Springfield St Suite 301   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXISYMMETRIC NOZZLES; AZIMUTHAL MODES; CONICAL NOZZLE; FAR-FIELD; FAR-FIELD NOISE; FREE JETS; HIGHER MODE; JET AXIS; LINEAR MICROPHONEARRAY; METHOD OF CHARACTERISTICS; NATURALLY OCCURRING; NOISE LEVELS; NOISE REDUCTIONS; NOZZLE EXITS; OVERALL SOUND PRESSURE LEVEL; PLASMA ACTUATOR; POLAR ANGLES; SCREECH TONES; SUPERSONIC JETS;

ACOUSTIC NOISE; ACTUATORS; NOZZLES; STROUHAL NUMBER;

SUPERSONIC AERODYNAMICS;

EID: 79954527808     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.4002811     Document Type: Article

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