Computational analysis of a pylon-chevron core nozzle interaction

7th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2001, Pages

  Thomas, Russell H ^a,c   Kinzie, Kevin W ^a,c   Paul Pao, S ^b,c  

^a Aeroacoustics Branch   (United States)

^b Building 45   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL ANALYSIS; DUAL-STREAM NOZZLES; FIELD PARAMETERS; FLOW DISTURBANCES; NOISE REDUCTION DEVICES; NOZZLE TRAILING EDGE; OPERATING POINTS; REYNOLDS AVERAGED NAVIER-STOKES EQUATION;

ACOUSTIC NOISE; AEROACOUSTICS; EXHAUST SYSTEMS (ENGINE); FLOW FIELDS; NAVIER STOKES EQUATIONS; NOISE ABATEMENT;

NOZZLES;

EID: 84896691346     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. st Century," Paper No. 6103 presented at the International Council of the Aeronautical Sciences.
2. th AIAA/CEAS Aeroacoustics Conference, June, 2000.
3. th Aerospace Sciences Meeting, January, 2000.
4. Khavaran, A., "Role of Anisotropy in Turbulent Mixing Noise," AIAA Journal, Vol. 37, No. 7, 1999, pp. 832-41.
5. Abdol-Hamid, K., "Development of a Three-Dimensional Code for the Analysis of Jet Mixing Problems," NASA CR 4200, 1988.