Turbulent flow field measurements of separate flow round and chevron nozzles with pylon interaction using Particle Image Velocimetry

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

Volumn 1, Issue , 2004, Pages 301-315

  Doty, Michael J ^a,b   Henderson, Brenda S ^a,c   Kinzie, Kevin W ^a,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Mail Stop 166 ^*  (United States)

^c Aeroacoustics Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CHEVRON NOZZLES; PARTICLE IMAGE VELOCIMETRY (PIV); PYLON INTERACTION; TURBULENT FLOW FIELD MEASUREMENTS;

ACOUSTIC NOISE; AIRCRAFT; AIRCRAFT PROPULSION; COMPUTATIONAL FLUID DYNAMICS; DATA ACQUISITION; HIGH TEMPERATURE EFFECTS; JET ENGINES; KINETIC ENERGY; NAVIER STOKES EQUATIONS; PRESSURE EFFECTS; REYNOLDS NUMBER; SHEAR STRESS; TURBULENT FLOW; VELOCITY MEASUREMENT;

NOZZLES;

EID: 19644366169     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Thomas, R. H., Kinzie, K. W., and Paul Pao, S., "Computational Analysis of a Pylon-Chevron Core Nozzle Interaction," AIAA Paper 2001-2185, May 2001.
2. Massey, S. and Thomas, R., "Computational and Experimental Flowfield Analyses of Separate Flow Chevron Nozzles and Pylon Interaction," AIAA Paper 2003-3212, May 2003.
3. Hunter, C. Pao, S. and Thomas, R., "Development of a Jet Noise Prediction Method for Installed Jet Configurations," AIAA Paper 2003-3169, May 2003.
4. Farassat, F., Doty, M. J., and Hunter, C., "The Acoustic Analogy - A Powerful Tool in Aeroacoustics with Emphasis on Jet Noise Prediction," AIAA Paper 2004-2872, May 2004.
5. Wernet, M. P., "PIVACQ Software Manual Version 2.2," NASA Glenn Research Center, January 2002.
6. Wernet, M. P., "Fuzzy Logic Enhanced Digital PIV Processing Software," NASA TM-1999-209274, 1999.
7. Bridges, J. and Wernet, M. P., "Turbulence Measurements of Separate Flow Nozzles with Mixing Enhancement Features," AIAA Paper 2002-2484, June 2002.
8. Birch, S. F., Lyubimov, D. A., Secundov, A. N., and Yakubovsky, K. Ya., "Numerical Modeling Requirements for Coaxial and Chevron Nozzle Flows," AIAA Paper 2003-3287, May 2003.
9. Bridges, J., "Measurements of Turbulent Flow Field in Separate Flow Nozzles with Enhanced Mixing Devices Test Report," NASA TM-2002-211366, 2002.
10. Thomas, R. and Kinzie K., "Jet-Pylon Interaction Effects for High Bypass Ratio Separate Flow and Chevron Nozzles," AIAA Paper 2004-2827, May 2004.