Method for separating shock wave motion and turbulence in LDV measurements

Experiments in Fluids

Volumn 26, Issue 4, 1999, Pages 358-370

  Palko, C W ^a   Dutton, J C ^b  

^a AEROSPACE CORPORATION   (United States)

^b University of Illinois at Urbana Champaign   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

LASER DOPPLER VELOCIMETERS; PRESSURE MEASUREMENT; SHOCK WAVES; TURBULENCE; UNSTEADY FLOW; WALL FLOW;

UNSTEADY OBLIQUE SHOCK WAVES;

SUPERSONIC FLOW;

EID: 0032663750     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s003480050299     Document Type: Article

References (29)

1. Adamson TC Jr; Messiter AF (1980) Analysis of two-dimensional interactions between shock waves and boundary layers. Ann Rev Fluid Mech 12: 103-138
2. Ardonceau PL (1984) The structure of turbulence in a supersonic shock-wave/boundary-layer interaction. AIAA J 22: 1254-1262
3. Bendat JS; Piersol AG (1986) Random data. New York: Wiley-Interscience
4. Beresh SJ; Clemens NT; Dolling DS; Comninos M (1997) Investigation of the causes of large-scale unsteadiness of shock-induced separated flow using planar laser imaging. AIAA paper 97-0064
5. Bloomberg JE (1989) An investigation of particle dynamics effects related to LDV measurements in compressible flows. M.S. Thesis, University of Illinois at Urbana-Champaign
6. Brown JD; Brown JL; Kussoy MI; Holt M; Horstman CC (1987) Two-component LDV investigation of three-dimensional shock/turbulent boundary layer interactions. AIAA paper 87-0553
7. Brusniak L (1988) Evaluation of conditional sampling methods for analysing separation shock motion. AIAA paper 88-0091
8. Chan SC; Clemens NT; Dolling DS (1995) Flowfield imaging of unsteady, separated compression ramp interactions. AIAA paper 95-2195
9. Dolling DS (1993) Fluctuating loads in shock wave/turbulent boundary layer interaction: tutorial and update. AIAA paper 93-0284
10. Dolling DS; Brusniak L (1989) Separation shock motion in fin, cylinder, and compression ramp-induced turbulent interactions. AIAA J 27: 734-742
11. Dolling DS; Murphy MT (1983) Unsteadiness of the separation shock wave structure in a supersonic compression ramp flowfield. AIAA J 21: 1628-1634
12. Dussauge JP; Dupont P (1995) Experimental evidences of compressibility effects on turbulence in high speed flows. In: Transitional and turbulent compressible flows. eds LD Kral; EF Spina; C Arakawa. ASME FED-Vol. 224, pp 185-192, ASME
13. Erengil ME; Dolling DS (1990) Correlation of separation shock motion in a compression ramp interaction with pressure fluctuations in the incoming boundary layer. AIAA paper 90-1646
14. Erengil ME; Dolling DS (1991) Unsteady wave structure near separation in a mach 5 compression ramp interaction. AIAA J 29: 728-735
15. Green JE (1970) Interactions between shock waves and turbulent boundary layers. Prog Aerospace Sci 11: 235-340
16. Herrin JL; Dutton JC (1993) An investigation of LDV velocity bias correction techniques for high-speed separated flows. Exp Fluids 15: 354-363
17. Herrin JL; Dutton JC (1995) The turbulence structure of a reattaching axisymmetric supersonic free shear layer. AIAA paper 95-2250
18. Jenson L (1991) Automatic digital signal processing for LDV. In: Proceedings of the 4th Int Conf on Laser Anemometry Advances and Applications. Vol. 2, pp 617-628, Cleveland, OH
19. Kuntz DW (1985) An experimental investigation of the shock wave-turbulent boundary layer interaction. Ph.D. Thesis, University of Illinois at Urbana-Champaign
20. Kussoy MI; Brown JD; Brown JL; Lockman WK; Horstman CC (1988) Fluctuations and massive separation in three-dimensional shock wave/boundary layer interactions. In: Transport phenomena in turbulent flows: theory, experiment, and numerical simulation. eds M Hirata; N Kasagi. pp 875-887, New York: Hemisphere
21. Liou T-M; Santavicca DA (1985) Cycle resolved LDV measurements in a motored IC engine. ASME Trans J Fluids Eng 107: 232-240
22. Palko CW (1998) Analyzed mean velocity and turbulence measurements in a conditionally plume-induced boundary layer separated flowfield. Ph.D. Thesis, University of Illinois at Urbana-Champaign
23. Palko CW; Dutton JC (1998) Velocity measurements in a shock-separated free shear layer. AIAA Paper 98-0698
24. Rask RB (1981) Comparison of window, smoothed-ensemble, and cycle-by-cycle data reduction techniques for laser doppler anemometer measurements of in-cylinder velocity. In: Fluid mechanics of combustion systems (eds T Morel; RP Lohmann; JM Rackley) pp 11-20, New York: ASME
25. Selig MS; Andreopoulos J; Muck KC; Dussauge JP; Smits AJ (1989) Turbulence structure in a shock wave/turbulent boundary layer interaction. AIAA J 27: 862-869
26. Selig MS; Smits AJ (1991) Effect of periodic blowing on attached and separated supersonic turbulent boundary layers. AIAA J 29: 1651-1658
27. Shaw RJ (1995) An experimental investigation of unsteady separation shock wave motion in a plume-induced, separated flowfield. Ph.D. Thesis, University of Illinois at Urbana-Champaign
28. Smits AJ; Muck KC (1987) Experimental study of three shock wave/turbulent boundary layer interactions. J Fluid Mech 182: 291-314
29. Witze PO; Martin JK; Borgnakke C (1984) Conditionally-sampled velocity and turbulence measurements in a spark ignition engine. Combust Sci Technol 36: 301-317