Abstract
The extension of particle image velocimetry to supersonic and hypersonic wind-tunnel flows has been achieved in the last decade. This was mainly possible with the advent of short interframing-time CCD cameras with temporal resolution allowing to obtain correlated particle images at flow velocities exceeding 1000m∕s. The most challenging aspects of PIV experiments in supersonic flows are still recognized as the seeding-particle-selection and seeding-distribution techniques. Also, the optical access for illumination and imaging require a specific attention since pressurized facilities offer limited optical access. The presence of shock waves in supersonic flows introduces regions where particle tracers slip with respect to the surrounding flow. Moreover, the particle seeding density becomes strongly nonuniform and particle-image blur can occur as a result of the strong refractive index variations. The present chapter reviews the physical and technical problems of PIV experiments and discusses the potential of such techniques on the basis of recent experiments performed in high-speed wind tunnels: double compression ramp at Mach 7 and shock-wave turbulent boundary interaction at Mach 2.
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References
G. Settles: Schlieren & Shadowgraph Techniques (Springer, Berlin, Heidelberg 2001)
D. Kastell, G. Eitelberg: A combined holographic interferometer and laser-schlieren system applied to high temperature, high velocity flows, in Instrumentation in Aerospace Simulation Facilities (ICIASF '95 Record, International Congress 18–21 1985) pp. 12/1–12/7
S. R. Sanderson, H. G. Hornung, B. Sturtevant: The influence of non-equilibrium dissociation on the flow produced by shock impingement on a blunt body, J. Fluid Mech. 516, 1–37 (2004)
V. A. Amatucci, J. C. Dutton, D. W. Kuntz, A. L. Addy: Two-stream, supersonic, wake flow field behind a thick base. {General} features, AIAA J. 30, 2039 (1992)
R. Benay, B. Chanetz, B. Mangin, L. Vandomme, J. Perraud: Shock wave/transitional boundary–layer interactions in hypersonic flow, AIAA J. 44, 1243–1254 (2006)
N. T. Clemens, M. G. Mungal: A planar {Mie} scattering technique for visualizing supersonic mixing flows, Exp. Fluids 11, 175 (1991)
N. T. Clemens, M. G. Mungal: Large scale structure and entrainment in the supersonic mixing layer, J. Fluid Mech. 284, 171 (1995)
R. J. Adrian: Twenty years of particle image velocimetry, in 12th Int. Symp. Appl. of Laser Tech. Fluid Mech. (2004)
A. J. Smits, J. P. Dussauge: Turbulent Shear Layers in Supersonic Flow (AIP Press 1996)
G. E. Elsinga, B. W. van Oudheusden, F. Scarano: Evaluation of optical distortion in {PIV}, Exp. Fluids 39 (2005)
C. S. Moraitis, M. L. Riethmuller: Particle image displacement velocimetry applied in high speed flows, in Proc. 4th Int. Symp. Appl. of Laser Anemometry to Fluid Dyn. (1988)
J. Kompenhans, R. H{ö}cker: Application of particle image velocimetry to high speed flows, in Riethmuller, M. L. (Eds.): Particle image displacement velocimetry, VKI Lecture Series (1988)
A. Krothapalli, D. P. Wishart, L. M. Lourenço: Near field structure of a supersonic jet: `on-line' {PIV} study, in Proc. 7th Int. Symp. Appl. of Laser Tech. Fluid Mech. (1994)
Lourenço, L. M.: Particle image velocimetry, in M. L. Riethmuller (Ed.): Particle Image Velocimetry, VKI Lecture Series 1996-03 (1996)
M. Raffel, H. H{ö}fer, F. Kost, C. Willert, J. Kompenhans: Experimental aspects of {PIV} measurements of transonic flow fields at a trailing edge model of a turbine blade, in Proc. 8th Int. Symp. Appl. of Laser Tech. Fluid Mech. (1996) paper No. 28.1.1
M. P. Wernet: Digital {PIV} measurements in the diffuser of a high speed centrifugal compressor, in (1998) {AIAA Paper No. 98-2777}
W. D. Urban, M. G. P. Mungal: Velocity measurements in compressible mixing layers, J. Fluid Mech. 431, 189 (2001)
F. Scarano, B. W. Van Oudheusden: Planar velocity measurements of a two-dimensional compressible wake, Exp. Fluids 34, 430–441 (2003)
F. Scarano: {PIV} image analysis for compressible turbulent flows. {Extension} of {PIV} to the hypersonic flow regime, particle tracers assessment, in Lecture Series on Advanced measuring techniques for Supersonic Flows (von Kármán Institute for Fluid Dynamics, Rhode-Saint Genèse 2005)
F. Scarano: Quantitative flow visualization in the high speed regime: {Heritage}, current trends and perspectives, in Proc. 12th Int. Symp. On Flow Vis. (2006) paper No. 2.1
R. A. Humble, F. Scarano, B. W. van Oudheusden, M. Tuinstra: {PIV} measurements of a shock wave/turbulent boundary layer interaction, in Proc. 13th Int. Symp. Appl. of Laser Tech. Fluid Mech. (2006)
J. Haertig, M. Havermann, C. Rey, A. George: Particle image velocimetry in {Mach} 3.5 and 4.5 shock-tunnel flows, AIAA J. 40, 1056 (2002)
F. F. J. Schrijer, F. Scarano, B. W. van Oudheusden: Application of {PIV} in a hypersonic double-ramp flow, in (2005) {AIAA paper No. 2005-3331}
A. Melling: Tracer particles and seeding for particle image velocimetry, Meas. Sci. Technol. 8, 1406 (1997)
G. Tedeschi, H. Gouin, M. Elena: Motion of tracer particles in supersonic flows, Exp. Fluids 26, 288 (1999)
S. A. Schaaf, P. L. Chambre: Fundamentals of Gas Dynamics (Princeton Univ. Press 1958)
J. L. Herrin, J. C. Dutton: Effect of a rapid expansion on the development of compressible free shear layers, Phys. Fluids 7, 159 (1995)
M. Samimy, S. K. Lele: Motion of particles with inertia in a compressible free shear layer, Phys. Fluids A 3, 1915 (1991)
F. F. J. Schrijer, F. Scarano, B. W. van Oudheusden: Application of {PIV} in a {Mach} 7 double-ramp flow, Exp. Fluids 41 (2006)
M. Raffel, C. Willert, J. Kompenhans: Particle Image Velocimetry, a Practical Guide (Springer, New York 1988)
G. E. Elsinga, B. W. van Oudheusden, F. Scarano: The effect of particle image blur on the correlation map and velocity measurement in {PIV}, in Optical Engineering and Instrumentation, SPIE Annual Meeting (2005)
M. Havermann, J. Haertig, C. Rey, A. George: Application of particle image velocimetry to high-speed supersonic flows in a shock tunnel, in 11th Int. Symp. on Applications of Laser Techniques to Fluid Mechanics, (2002)
W. L. Hankey, Jr, M. S. Holden: Two-dimensional shock-wave boundary layer interactions in high speed flows, in AGARDograph, vol. 203 (1975)
J. D{\'e}lery, J. G. Marvin: Shock-wave boundary layer interactions, in AG 280, AGARD (1986)
K. Sinha, M. J. Wright, G. V. Candler: The effect of turbulence on double-cone shock interactions, in (1999) {AIAA paper No. 99-0146}
D. S. Dolling: Fifty years of shock wave/boundary layer interation research: What next?, AIAA J. 39 (2001)
R. Theunissen, F. F. J. Schrijer, F. Scarano, M. L. Riethmuller: Application of adaptive {PIV} interrogation in a hypersonic flow, in Proc. 13th Int. Symp. Appl. of Laser Tech. Fluid Mech. (2006)
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Scarano, F. (2007). Overview of PIV in Supersonic Flows. In: Particle Image Velocimetry. Topics in Applied Physics, vol 112. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-73528-1_24
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DOI: https://doi.org/10.1007/978-3-540-73528-1_24
Publisher Name: Springer, Berlin, Heidelberg
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