Parametric testing of chevrons on single flow hot jets

Collection of Technical Papers - 10th AIAA/CEAS Aeroacoustics Conference

Volumn 1, Issue , 2004, Pages 284-300

  Bridges, James ^a   Brown, Clifford A ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CHEVRONS; GEOMETRIC PARAMETERS; PHYSICS-BASED NOISE; SINGLE FLOW NOZZLES;

ACOUSTIC NOISE; DATABASE SYSTEMS; GRADIENT METHODS; JET ENGINES; MATHEMATICAL MODELS; NOISE ABATEMENT; OPTIMIZATION; TURBULENCE; VIBRATIONS (MECHANICAL);

NOZZLES;

EID: 19644375797     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Saiyed, N., Mikkelsen, K.L., and Bridges, J., 2000, "Acoustics and Thrust of Separate-Flow Exhaust Nozzles With Mixing Devices for High-Bypass-Ratio Engines," NASA TM 2000-209948.
2. th AIAA/CEAS Aeroacoustics Conference, Breckenridge, CO, (AIAA-2002-2484).
3. th AIAA/CEAS Aeroacoustics Conference, Hiltonhead, NC, (AIAA-2003-3130).
4. Tanna, H.K., "The influence of temperature on shock-free supersonic jet noise", J Sound Vibration Vol. 39 1975
5. th AIAA/CEAS Aeroacoustics Conference, Manchester, UK, (AIAA-2004-2896).