Aeroacoustic measurements of a wing/slat model

8th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Mendoza, Jeff M ^a   Brooks, Thomas F ^b,c   Humphreys, William M ^b,d  

^a HONEYWELL   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Aeroacoustics Branch   (United States)

^d Advanced Measurement and Diagnostics Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; BOUNDARY LAYERS; NASA; WINGS;

ACOUSTIC DATABASE; ACOUSTIC MEASUREMENTS; AEROACOUSTIC MEASUREMENTS; DISTRIBUTED NOISE; HIGH-LIFT DEVICES; NASA LANGLEY RESEARCH CENTER; TRAILING EDGE NOISE; WING LEADING EDGES;

AEROACOUSTICS;

EID: 85085404484     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-2604     Document Type: Conference Paper

References (21)

1. Macaraeg, M. G., "Fundamental Investigations of Airframe Noise", AIAA Paper 98-2224, June 1998.
2. Davy, R., and Remy, H., "Airframe Noise Characteristics on a 1/11 Scale Airbus Model", AIAA Paper 98-2335, June 1998.
3. Hayes, J. A., Horne, C. W., Soderman, P. T., and Bent, P. H., "Airframe Noise Characteristics of a 4. 7% Scale DC-10 Model", AIAA Paper 97-1594-CP, 3rd AIAA/CEAS Aeroacoustics Conference and Exhibit, Atlanta, GA, May, 1997.
4. th AIAA/CEAS Aeroacoustics Conference and Exhibit, Bellevue, WA, May, 1999.
5. Guo, Y. P., Hardy, B., Bent, P., Yamamoto, K., and Joshi, M., "Surface Pressure Fluctuations on DC-10 High Lift System and their Correlation with Far Field Noise", NASI-20103, Task 2, NASA CRAD-9310-4872, 1998.
6. Guo, Y. P., Hardy, B., Bent, P., Yamamoto, K., and Joshi, M., "Noise Characteristics of DC-10 Aircraft High Lift Systems", NASI-20103, Task 2, NASA CRAD-9310-4893, 1998.
7. th AIAA/CEAS Aeroacoustics Conference, Maastricht, Netherlands, May, 2001.
8. Thomas, F. O., Nelson, R. C., and Lui, X., "Experimental Investigation of the Confluent Boundary Layer of a High-Lift System", AIAA Journal, Volume 38, Number 6, pp. 978-988, June, 2000.
9. rd International Workshop on PIV, 1999.
10. th AIAA/CEAS Aeroacoustics Conference and Exhibit, Bellevue, WA, May, 1999.
11. Guo, Y. P., "A Model for Slat Noise Generation", AIAA Paper 97-1647, 3rd AIAA/CEAS Aeroacoustics Conference and Exhibit, Atlanta, GA, May, 1997.
12. th AIAA/CEAS Aeroacoustics Conference and Exhibit, Bellevue, WA, May, 1999.
13. Singer, B. A., Lockard, D. P., Brentner, K. S., Khorrami, M. R., Berkman, M. E., and Choudhari, M, "Computational Aeroacoustic Analysis of Slat Trailing Edge Flow", AIAA Paper 99-1802, 5th AIAA/CEAS Aeroacoustics Conference and Exhibit, Bellevue, WA, May, 1999.
14. th AIAA/CEAS Aeroacoustics Conference and Exhibit, Maastricht, Netherlands, May, 2001.
15. th AIAA/CEAS Aeroacoustics Conference and Exhibit, Maastricht, The Netherlands, May, 2001.
16. Humphreys, W. M., Brooks, T. F., Hunter, W. W., and Meadows, K. R., "Design and Use of Microphone Directional Arrays for Aeroacoustic Measurements", AIAA Paper 98-0471, 36st Aerospace Science Meeting and Exhibit, Reno, NV, January, 1998.
17. rd AIAA/CEAS Aeroacoustics Conference, Atlanta, GA, May, 1997.
18. th Aeroacoustics Conference, Bellevue, WA, May, 1999.
19. Brooks, T. F., and Humphreys, W. M., "Flap Edge Aeroacoustic Measurements and Predictions", AIAA paper 2000-1975, 6th AIAA/CEAS Aeroacoustics Conference, Lahaina, Hawaii, June, 2000.
20. Lilley, G. M., "The Prediction of Airframe Noise and Comparison with Experiment", Journal of Sound and Vibration, 239(4), pp. 849-859, 2001.
21. Brooks, T. F., Pope, D. S., Marcolini, M. A., "Airfoil Self-Noise and Prediction", NASA Reference Publication 1218, July, 1989.