Turbulence correlation length-scale relationships for the prediction of aeroacoustic response

AIAA Journal

Volumn 43, Issue 6, 2005, Pages 1187-1197

  Lynch III, Denis A ^a,c   Blake, William K ^a,c   Mueller, Thomas J ^b,d  

^a NAVAL SURFACE WARFARE CENTER   (United States)

^b UNIVERSITY OF NOTRE DAME   (United States)

^c Carderock Division   (United States)

^d Department of Aerospace and Mechanical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC ACOUSTICS; FOURIER TRANSFORMS; MATHEMATICAL MODELS; PRESSURE EFFECTS; STATORS; TIME DOMAIN ANALYSIS; TURBULENCE; TURBULENT FLOW;

AEROACOUSTIC RESPONSE; DYNAMIC PRESSURE; TURBULENCE CORRELATION; WAVE NUMBER;

AERODYNAMICS;

EID: 20444455098     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.2200     Document Type: Article

References (29)

1. von Kármán, T., and Sears, W. R., "Airfoil Theory for Non-Uniform Motion," Journal of the Aeronautical Sciences, Vol. 5, No. 10, 1938, pp. 379-390.
2. Sears, W. R., "Some Aspects of Non-Stationary Airfoil Theory and Its Practical Application," Journal of the Aeronautical Sciences, Vol. 8, No. 3, 1941, pp. 104-108.
3. Blake, W. K., Mechanics of Flow Induced Sound and Vibration, Wiley, New York, 1986.
4. Amiet, R. K., "Acoustic Radiation from an Airfoil in a Turbulent Stream," Journal of Sound and Vibration, Vol. 41, No. 4, 1975, pp. 407-420.
5. Wygnanski, I., Champagne, F., and Marasli, B., "On the Large-Scale Structures in Two-Dimensional Small-Deficit, Turbulent Wakes," Journal of Fluid Mechanics, Vol. 168, 1986, pp. 31-71.
6. Glegg, S. A. L., "Prediction of Blade Wake Interaction Noise Based on a Turbulent Vortex Model," AIAA Journal, Vol. 29, No. 10, 1991, pp. 1545-1551.
7. Devenport, W. J., Wenger, C. W., Glegg, S. A. L., and Miranda, J. A., "Wave Number Frequency Spectra of a Lifting Wake for Broadband Noise Prediction," AIAA Journal, Vol. 36, No. 6, 1998, pp. 881-887.
8. Devenport, W. J., Muthanna, C., Ma, R., and Glegg, S. A. L., "Two-Point Descriptions of Wake Turbulence with Application to Noise Prediction," AIAA Journal, Vol. 39, No. 12, 2001, pp. 2302-2307.
9. Glegg, S. A. L., Wittmer, K. S., Devenport, W. J., and Pope, D.S., "Broadband Helicopter Noise Generated by Blade Wake Interactions," Journal of the American Helicopter Society, Vol. 44, No. 4, 1999, pp. 293-301.
10. Wojno, J. P., "An Experimental Investigation of the Aeroacoustic Response of a Ten-Bladed Rotor Ingesting Grid-Generated Turbulence," Ph.D. Dissertation, Dept. of Aerospace and Mechanical Engineering, Univ. of Notre Dame, Notre Dame, IN, 1999.
11. Panton, R. L., and Linebarger, J. H., "Wall Pressure Spectra Calculations for Equilibrium Boundary Layers," Journal of Fluid Mechanics, Vol. 65, No. 2, 1974, pp. 261-287.
12. Hinze, J. O., Turbulence, McGraw-Hill, New York, 1975.
13. Gradshteyn, I. S., and Ryzhik, I. M., Table of Integrals, Series, and Products, Academic Press, New York, 1980.
14. Mueller, T. J., Scharpf, D. F., Batill, S. M., Strebinger, R. B., Sullivan, C. J., and Subramanian, S., "The Design of a Low-Noise, Low-Turbulence Wind Tunnel for Acoustic Measurements," AIAA Paper 92-3883, July 1992.
15. Mueller, T. J., Scharpf, D. F., Batill, S. M., Strebinger, R. B., Sullivan, C. J., and Subramanian, S., "A New Low Speed Wind Tunnel for Acoustic Measurements," Proceedings of the European Forum on Wind Tunnels and Wind Tunnel Test Techniques, Royal Aeronautical Society, London, 1992.
16. Lynch, D. A., III, "An Experimental Investigation of the Unsteady Response of a Stator Located Downstream of a Propeller Ingesting Broadband Turbulence," Ph.D. Dissertation, Dept. of Aerospace and Mechanical Engineering, Univ. of Notre Dame, Notre Dame, IN, 2001.
17. Lynch, D. A., III, Mueller, T. J., and Blake, W. K., "Aeroacoustic Response of an Airfoil Downstream of a Propeller Ingesting Broadband Turbulence," AIAA Paper 2001-2240, May 2001.
18. Kaji, S., and Okazaki, T., "Generation of Sound by Rotor-Stator Interaction," Journal of Sound and Vibration, Vol. 13, No. 3, 1970, pp. 281-307.
19. Falk, E. A., "An Experimental Investigation of Aerodynamic Forcing in the F109 Turbofan Engine Compressor," Ph.D. Dissertation, Dept. of Aerospace and Mechanical Engineering, Univ. of Notre Dame, Notre Dame, IN, 2000.
20. Corcos, G. M., "The Structure of the Turbulent Pressure Field in Boundary-Layer Flows," Journal of Fluid Mechanics, Vol. 18, 1964, pp. 353-378.
21. Dryden, H. L., "Turbulence Investigations at the National Bureau of Standards," Proceedings of the 5th International Congress of Applied Mathematics, 1938.
22. Bendat, J. S., and Piersol, A. G., Random Data: Analysis and Measurement Procedures, Wiley, New York, 2000.
23. Lynch, D. A., III, Blake, W. K., and Mueller, T. J., "Turbulent Flow Downstream of a Propeller, Part 1: Wake Turbulence," AIAA Journal, Vol. 43, No. 6, 2005, pp. 1198-1210.
24. Lynch, D. A., III, Blake, W. K., and Mueller, T. J., "Turbulent Flow Downstream of a Propeller, Part 2: Ingested, Propeller-Modified Turbulence," AIAA Journal, Vol. 43, No. 6, 2005, pp. 1211-1220.
25. Scharpf, D. F., "An Experimental Investigation of the Sources of Propeller Noise Due to Turbulence Ingestion," Ph.D. Dissertation, Dept. of Aerospace and Mechanical Engineering, Univ. of Notre Dame, Notre Dame, IN, 1993.
26. Minniti, R. J., III, Blake, W. K., and Mueller, T. J., "Inferring Propeller Inflow and Radiation from Near-Field Response, Part 1: Analytic Development," AIM Journal, Vol. 39, No. 6, 2001, pp. 1030-1036.
27. Minniti, R. J., III, Blake, W. K., and Mueller, T. J., "Inferring Propeller Inflow and Radiation from Near-Field Response, Part 2: Empirical Application," AIAA Journal, Vol. 39, No. 6, 2001, pp. 1037-1046.
28. Wojno, J. P., Mueller, T. J., and Blake, W. K., "Rotor Turbulence Ingestion Noise, Part 1: Experimental Characterization of Grid-Generated Turbulence," AIAA Journal, Vol. 40, No. 1, 2002, pp. 16-25.
29. Wojno, J. P., Mueller, T. J., and Blake, W. K., "Rotor Turbulence Ingestion Noise, Part 2: Rotor Aeroacoustic Response," AIAA Journal, Vol. 40, No. 1, 2002, pp. 26-32.