Measurements and predictions for a distributed exhaust nozzle

7th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2001, Pages

  Kinzie, Kevin W ^a   Brown, Martha C ^a   Schein, David B ^b   Solomon Jr , W David ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC MEASUREMENTS; AERO-DYNAMIC PERFORMANCE; CFD APPROACHES; DESIGN CONCEPT; DESIGN METHODOLOGY; DESIGN TOOL; DISTRIBUTED EXHAUST NOZZLES; REFERENCE NOZZLES;

AEROACOUSTICS; AERODYNAMICS; DESIGN; FORECASTING; NOISE ABATEMENT; NOZZLES;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84896843857     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Schein, D. B., Hausmann, J. S., Ybarra, A. H., and Smith, D. L., "Design and Demonstration of a Flight Worthy, Very Low Jet Mixing Noise Exhaust System," Final Report, NASA Contract No. NAS3-25816, Task 16.
2. th AIAA Fluid Dynamics Conference, June, 1996.
3. th AIAA/CEAS Aeroacoustics Conference, June, 2000.
4. Brooks, T. F., Pope, S. D., and Marcolini, M. A., "Airfoil Self-Noise and Prediction," NASA RP-1218, 1989.