Experiment to Support the Formulation and Validation of Compressor-Face Boundary Conditions

Journal of Propulsion and Power

Volumn 16, Issue 3, 2000, Pages 406-414

  Freund, Donald ^a   Sajben, Miklos ^b  

^a GULFSTREAM AEROSPACE CORPORATION   (United States)

^b UNIVERSITY OF CINCINNATI   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000291158     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5604     Document Type: Article

References (44)

1. Mattingly, J. D., Heiser, W. H., and Daley, D. H., Aircraft Engine Design, American Inst. of Aeronautics and Astronautics, New York, 1987, p. 381.
2. Domack, C. S., "A Preliminary Investigation of Inlet Unstart Effects on a High-Speed Civil Transport Concept," AIAA Paper 91-3327, Sept. 1991.
3. Clark, L. T., "Dynamic Response Characteristics of a Mixed Compression Supersonic Inlet as a Part of a Larger System," AIAA Paper 95-0036, Jan. 1995.
4. Chung, J., "Numerical Simulation of a Mixed-Compression Supersonic Inlet Flow," AIAA Paper 94-0583, Jan. 1994.
5. Chung, J., and Cole, G. L., "Comparison of Compressor Face Boundary Conditions for Unsteady CFD Simulations of Supersonic Inlets," AIAA Paper 95-2627, July 1995.
6. Decher, R., Mayer, D. W., and Paynter, G. C., "On Supersonic Inlet-Engine Stability," AIAA Paper 94-3371, July 1994.
7. Mayer, W. D., and Paynter, G. C., "Prediction of Supersonic Inlet Unstart Caused by Freestream Disturbances," AIAA Journal, Vol. 33, No. 2, 1995, pp. 256-275.
8. Mayer, W. D., and Paynter, G. C., "Boundary Conditions for Unsteady Supersonic Inlet Analyses," AIAA Journal, Vol. 32, No. 6, 1994, pp. 1200-1206.
9. Paynter, G. C., Mayer, D. W., and Tjonneland, E., "Flow Stability Issues in Supersonic Inlet Flow Analyses," AIAA Paper 93-0290, Jan. 1993.
10. Saunders, J. D., and Keith, T. G., "Results From Computational Analysis of Mixed Compression Supersonic Inlet," AIAA Paper 91-2581, 1991.
11. Numbers, K., and Hamed, A., "Development of a Coupled Inlet-Engine Dynamic Analysis Method," AIAA Paper 97-2880, July 1997.
12. Sugiyama, Y., Tabakoff, W., and Hamed, A., "J85 Surge Transient Simulation," Journal of Propulsion and Power, Vol. 5, No. 3, 1989, pp. 375-381.
13. Cole, G. L., "Atmospheric Effects on Inlets for Supersonic Cruise Aircraft," AIAA Paper 77-874, July 1977.
14. Wasserbauer, J. F., and Whipple, D. L., "Experimental Investigation of the Dynamic Response of a Supersonic Inlet to External and Internal Disturbances," NASA TM X-1648, Sept. 1968.
15. Baumbick, R. J., Wallhagen, R. E., Neiner, G. H., and Batterton, P. G., "Dynamic Response of Mach 2.5 Axisymmetric Inlet with 40 Percent Supersonic Internal Area Contraction," NASA TM X-2833, July 1973.
16. Sanders, B. W., "Dynamic Response of a Mach 2.5 Axisymmetric Inlet and Turbojet Engine with a Poppet-Valve-Controlled Inlet-Stability Bypass System when Subjected to Internal and External Airflow Transients," NASA TP-1531, Jan. 1980.
17. Wasserbauer, J. F., "Dynamic Response of a Mach 2.5 Axisymmetric Inlet with Engine or Cold Pipe and Utilizing 60 Percent Supersonic Internal Area Contraction," NASA TN D-5338, July 1969.
18. Brimelow, B., Collins, T. P., and Pfefferkorn, G. A., "Engine Testing in a Dynamic Environment," AIAA Paper 74-1198, Oct. 1974.
19. Melick, H. C., "Analysis of Inlet Flow Distortion and Turbulence Effects on Compressor Stability," NASA TR CR-114577, March 1973.
20. Das, D. K., and Trippi, A., "Effects of Inlet Pressure Fluctuations on Axial Flow Compressors," Journal of Propulsion and Power, Vol. 5, No. 1, 1989, pp. 72-81.
21. Kurkov, A. P., Soeder, R. H., and Moss, J. E., "Investigation of the Stall Hammershock at the Engine Inlet," Journal of Aircraft, Vol. 12, No. 4, 1975, pp. 198-204.
22. Marshall, F. L., "Prediction of Inlet Duct Overpressures Resulting from Engine Surge," Journal of Aircraft, Vol. 10, No. 5, 1973, pp. 274-278.
23. Ferri, A., and Nucci, L. M., "The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions," NACA RM L50K30, Jan. 1951.
24. Kovasznay, L. S. G., "Turbulence in Supersonic Flow," Journal of the Aeronautical Sciences, Vol. 20, No. 10, 1953, pp. 657-675.
25. Reynolds, G. G., Vier, W. F., and Collins, T. P., "An Experimental Evaluation of Unsteady Flow Effects on an Axial Compressor - P3 Generator Program," U.S. Air Force Aero Propulsion Lab. Technical Rep. AFAPL-TR-73-43, Wright-Patterson AFB, OH, July 1973.
26. Peacock, R. E., "An Experimental Study of Pulsating Flow in a Three-Stage Axial Flow Compressor," Proceedings of the Winter Annual Meeting, American Society of Mechanical Engineers, San Francisco, CA, Dec. 1978, pp. 185-191.
27. Kaji, S., and Okazaki, T., "Propagation of Sound Waves Through a Blade Row: I. Analysis Based on the Semi-Actuator Disk Theory," Journal of Sound and Vibration, Vol. 11, No. 3, 1970, pp. 339-353.
28. Kaji, S., and Okazaki, T., "Propagation of Sound WavesThrough a Blade Row: II. Analysis Based on the Acceleration Potential Method," Journal of Sound and Vibration, Vol. 11, No. 3, 1970, pp. 355-370.
29. Paynter, G. C., Clark, L. T., and Cole, G. L., "Modeling the Response from a Cascade to an Upstream Acoustic Disturbance," AIAA Paper 98-0953, Jan. 1998.
30. Paynter, G. C., "Response of a Two-Dimensional Cascade to an Upstream Disturbance," AIAA Journal, Vol. 35, No. 3, 1997, pp. 434-440.
31. Freund, D. D., "Experimental Exploration of Compressor-Face Boundary Conditions for Unsteady Inlet Flow Computations," Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Cincinnati, Cincinnati, OH, Dec. 1997.
32. Freund, D., and Sajben, M., "Reflection of Large Amplitude Acoustic Pulses from an Axial Flow Compressor," AIAA Paper 97-2879, July 1997.
33. Freund, D., and Sajben, M., "Experimental Investigation of Outflow Boundary Conditions Used in Unsteady Inlet Flow Computations," AIAA Paper 97-0610, Jan. 1997.
34. Freund, D., and Sajben, M., "Compressor-Face Boundary Condition Experiment: Generation of Acoustic Pulses in Annular Ducts," AIAA Paper 96-2657, July 1996.
35. Sajben, M., and Freund, D. D., "Experimental Exploration of Compressor-Face Boundary Conditions for Unsteady Inlet Flow Computations," AIAA Paper 95-2886, July 1995.
36. Chung, J. Y., and Blaser, D. A., "Transfer Function Method of Measuring In-Duct Acoustic Properties. Part II, Experiment," Journal of the Acoustic Society of America, Vol. 68, No. 3, 1980, pp. 914-921.
37. "Standard Test Method for Impedance and Absorption of Acoustic Materials Using a Tube, Two Microphones, and a Digital Frequency Analysis System," ASTM Standard: E1050-98, American Society for Testing and Materials, West Conshohocken, PA, May 1998.
38. Singh, R., and Katra, T., "Development of an Impulse Technique for Measurement of Muffler Characteristics," Journal of Sound and Vibration, Vol. 56, No. 2, 1978, pp. 279-298.
39. Salikuddin, M., and Mungur, P., "Acoustic Radiation Impedance of Duct-Nozzle System," Journal of Sound and Vibration, Vol. 86, No. 4, 1981, pp. 497-522.
40. Salikuddin, M., and Plumblee, H. E., "Low Frequency Sound Absorption of Orifice Plates and Nozzles," AIAA Paper 80-0991, June 1980.
41. Bendat, J. S., and Piersol, A. G., Engineering Applications or Correlation and Spectral Analysis, Wiley, New York, 1980, p. 67.
42. Ozyoruk, Y., and Long, L., "A Time-Domain Implementation of Surface Acoustic Impedance Condition with and without Flow," AIAA Paper 96-1663, May 1996.
43. Ozyoruk, Y., and Long, L., "Impedance Boundary Conditions for Time-Domain Computational Aeroacoustics Methods," AIAA Paper 97-0021, Jan. 1997.
44. Tam, C. K. W., and Auriault, L., "Time-Domain Impedance Boundary Conditions for Computational Aeroacoustics," AIAA Journal, Vol. 34, No. 5, 1996, pp. 917-923.