Installation effects on coaxial jet noise - An experimental study

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Blackner, A M ^a   Bhat, T R S ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE MEASUREMENT; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; ENGINES; INSTALLATION; WIND TUNNELS; WINGS;

ANECHOIC WIND TUNNELS; COMMERCIAL TRANSPORT; ENGINE CONFIGURATION; EXPERIMENTAL PROGRAM; INSTALLATION EFFECTS; INSTALLATION LOCATIONS; NOISE SUPPRESSORS; WING LEADING EDGES;

JET AIRCRAFT;

EID: 85088193608     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-80     Document Type: Conference Paper

References (4)

1. Shivashankara, B. N. and Blackner, A. M., "Installed Jet Noise," AIAA 97-1601, 3rd AIAA/CEAS Aeroacoustics Conference, Atlanta, GA, May 1997.
2. Underbrink, J. R. and Dougherty, R. R, "Array Design for Non-Intrusive Measurement of Noise Sources," Proceedings of Noise-Con 96, page 757, Seattle, WA, September 1996.
3. Bhat, T. R. S., Blackner, A. M., "Installed Jet Noise Prediction Model for Coaxial Jets," AIAA 98-0079, 36th AIAA Aerospace Sciences Meeting, Reno, NV, January 1998.
4. Lu, H. Y., "An empirical model for prediction of coaxial jet noise in ambient flow," AIAA 86-1912, AIAA 10th Annual Aeroacoustics Conference, Seattle, WA, July 1986.