Low frequency noise contamination in fan model testing

Proceedings of the ASME Turbo Expo

Volumn 6, Issue PART A, 2008, Pages 849-861

  Brown, Clifford A ^a   Schifer, Nicholas A ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DATA QUALITY; EFFECTIVE PERCEIVED NOISE LEVELS; ENGINE COMPONENTS; EXIT VELOCITY; FAN NOISE; FREE STREAM; JET NOISE; LEAST SQUARES FIT; LOW-FREQUENCY NOISE; LOW-SPEED WIND TUNNEL; MODEL TESTING; NASA GLENN; NOISE COMPONENTS; NOISE CONTAMINATION; NOISE DATA; NOISE SOURCE; NOZZLE PRESSURE RATIO; POWER LEVELS; PYLON INTERACTION; RESEARCH AND DEVELOPMENT; SCALE MODELS;

ACOUSTIC NOISE MEASUREMENT; AIRCRAFT; AIRCRAFT ENGINES; INSTALLATION; JETS; MATHEMATICAL MODELS; NASA; WIND TUNNELS;

ACOUSTIC NOISE;

EID: 69949138211     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2008-50850     Document Type: Conference Paper

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