Abstract
Experiments were performed within Rutgers University’s supersonic wind tunnel to measure the influence of off-axis laser energy deposition on the flow field about an ogive cylinder at a freestream Mach number of 3.4. Perturbation of the flow field was accomplished using an infrared laser source, focused to a point ahead of the ogive cylinder. Stereoscopic particle image velocimetry measurements were performed to quantify the effects of energy deposition on the flow field at discrete time delays following the generation of the spark. The SPIV results showed a measurable change in streamwise velocity downstream of ogive’s shock that appears to be dependent on proximity of the initial spark to the ogive’s surface. In contrast, the spark was shown to have little influence on the vertical velocity component at early times. Data corresponding to later times showed the passage of an induced jet through the flow field. The jet rotated about its axis while passing through the shock structure, in agreement with previous qualitative imaging. These results demonstrate the feasibility of using SPIV to investigate the influence of laser energy deposition on the flow field.
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Adelgren R, Yan H, Elliott G, Knight D, Beutner T, Zheltovodov A (2005) Control of edney iv interaction by pulsed laser energy deposition. AIAA J 43(2):256–269
Adelgren RG (2002) Localized flow control with energy deposition. PhD thesis, Rutgers, The State University of New Jersey
Alberti A, Munafò A, Pantano C, Panesi M (2020) Self-consistent computational fluid dynamics of supersonic drag reduction via upstream-focused laser-energy deposition. AIAA J. https://doi.org/10.2514/1.J059612
Anderson KV, Knight DD (2012) Plasma jet for flight control. AIAA J 50(9):1855–1872
Aure R, Jacobs JW (2008) Particle image velocimetry study of the shock-induced single mode Richtmyer-Meshkov instability. Shock Waves 18(3):161–167
Belinger A, Hardy P, Barricau P, Cambronne JP (2011) Influence of the energy dissipation rate in the discharge of a plasma synthetic jet actuator. J Phys D 44:365201. https://doi.org/10.1088/0022-3727/44/36/365201
Bletzinger P, Ganguly BN, Van Wie D, Garscadden A (2005) Plasmas in high speed aerodynamics. J Phys D: Appl Phys 38:R33–R57
Bright A, Tichenor N, Kremeyer K, Wlezien R (2018) Boundary-layer separation control using laser-induced air breakdown. AIAA J 56(4):1472–1482
Buschbeck M, Bittner N, Halfmann T, Arndt S (2012) Dependence of combustion dynamics in a gasoline engine upon the in-cylinder flow field, determined by high-speed piv. Exp Fluids 53(6):1701–1712
Caruana D, Barricau P, Hardy P, Cambronne JP, Belinger A (2009) The ‘plasma synthetic jet’ actuator. aero-thermodynamic characterization and first flow control applications. AIAA Paper 2009-1307 https://doi.org/10.2514/6.2009-1307
Chen X, Bian B, Shen Z, Lu J, Ni X (2003) Equations of laser-induced plasma shock wave motion in air. Microw Opt Technol Lett 38(1):75–79
Emerick T, Ali MY, Foster C, Alvi FS, Popkin S (2014) Sparkjet characterizations in quiescient and supersonic flowfields. Exp Fluids 55:1858
Fomin VM, Tretyakov PK, Taran JP (2004) Flow control using various plasma and aerodynamic approaches (short review). Aerosp Sci Technol 8(5):411–421. https://doi.org/10.1016/j.ast.2004.01.005
Glumac N, Elliott G (2007) The effect of ambient pressure on laser-induced plasmas in air. Opt Lasers Eng 45(1):27–35
Grossman KR, Cybyk BZ, VanWie DM (2003) Sparkjet actuators for flow control. AIAA Paper No 2003-57
Iwakawa A, Shoda T, Pham HS, Tamba T, Sasoh A (2016) Suppression of low-frequency shock oscillations over boundary layers by repetitive laser pulse energy deposition. Aerospace 3(2):13
Kianvashrad N, Knight D (2019) Numerical simulation of laser energy discharge for flight control. J Phys D: Appl Phys 52(49):494005
Kianvashrad N, Knight D, Wilkinson SP, Chou A, Horne RA, Herring GC, Beeler GB, Jangda M (2018) Effect of off-body laser discharge on drag reduction of hemisphere cylinder in supersonic flow-part II. AIAA Paper No 2018-1433
Kim JH, Matsuda A, Sakai T, Sasoh A (2011) Wave drag reduction with acting spike induced by laser-pulse energy deposition. AIAA J 49(9):2076–2078
Knight D (2008) Survey of aerodynamic drag reduction at high speed by energy deposition. J Propul Power 24(6):1153–1167
Knight D (2013) A summary of laser and microwave flow control in high-speed flows. Prog Flight Phys 5:125–138
Ko HS, Haack SJ, Land HB, Cybyk B, Katz J, Kim HJ (2010) Analysis of flow distribution from high-speed flow actuator using particle image velocimetry and digital speckle tomography. Flow Meas Instrum 21:443–453
Kontis K (2014) Development and application of laser-induced energy deposition for flow control of Edney Type IV interactions. Final Report FA8655-12-1-2007, University of Manchester Research Office
Kopecek H, Maier H, Reider G, Winter F, Wintner E (2003) Laser ignition of methane-air mixtures at high pressures. Exp Therm Fluid Sci 27(4):499–503
Kremeyer K (2015a) Energy deposition I: application to revolutionize high speed flight and flow control. AIAA Paper No 2015-3560
Kremeyer K (2015b) Energy deposition II: physical mechanisms underlying techniques to achieve high-speed flow control. AIAA Paper No 2015-3502
Lazar E, Elliott G, Glumac N (2008) Control of the shear layer above a supersonic cavity using energy deposition. AIAA J 46(12):2987–2997
Lazar E, Elliott G, Glumac N (2009) Energy deposition applied to a transverse jet in a supersonic crossflow. AIAA Paper No 2009-1534
Leonov SB (2011) Review of plasma-based methods for high-speed flow control. AIP Conf Proc 1376:498–502
Leonov SB, Yarantsev DA (2008) Near-surface electrical discharge in supersonic airflow: properties and flow control. AIAA J 24(6):1168–1181
Merriman S, Ploenjes E, Palm P, Adamovich IV (2001) Shock wave control by nonequilibrium plasmas in cold supersonic gas flows. AIAA J 39(8):1547–1552
Narayanaswamy V (2010) Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control. PhD thesis, The University of Texas at Austin
Narayanaswamy V, Raja LL, Clemens NT (2012a) Control of a shock/boundary-layer interaction by using a pulsed-plasma jet actuator. AIAA J 50(1):246–249. https://doi.org/10.2514/1.J051246
Narayanaswamy V, Raja LL, Clemens NT (2012b) Control of unsteadiness of a shock wave/turbulent boundary layer interaction by using a pulsed-plasma-jet actuator. Phys Fluids 24:076101. https://doi.org/10.1063/1.4731292
Nishihara M, Takashima K, Rich JW, Adamovich IV (2011) Mach 5 bow shock control by a nanosecond pulse surface dielectric barrier discharge. Phys Fluids 23:066101
Nishihara M, Freund JB, Glumac NG, Elliott GS (2018) Influence of mode-beating pulse on laser-induced plasma. J Phys D: Appl Phys 51:135601
Osuka T, Erdem E, Hasegawa N, Majima R, Tamba T, Yokota S, Sasoh A, Kontis K (2014) Laser energy deposition effectiveness on shock-wave boundary-layer interactions over cylinder-flare combinations. Phys Fluids 26:096103
Panco RB, DeMauro EP (2020) Measurements of a mach 3.4 turbulent boundary layer using stereoscopic particle image velocimetry. Exp Fluids 61(4):107
Pham HS, Shoda T, Tamba T, Iwakawa A, Sasoh A (2017) Impacts of laser energy deposition on flow instability over double-cone model. AIAA J 55(9):2992–3000
Phuoc TX (2006) Laser-induced spark ignition fundamental and applications. Opt Lasers Eng 44(5):351–397
Russell A, Zare-Behtash H, Kontis K (2016) Joule heating flow control methods for high-speed flows. J Electrost 80:34–68
Samimy M, Lele SK (1991) Motion of particles with inertia in a compressible free shear layer. Phys Fluids 3(8):1915. https://doi.org/10.1063/1.857921
Samimy M, Adamovich I, Webb B, Kastner J, Hileman J, Keshav S, Palm P (2004) Development and characterization of plasma actuators for high-speed jet control. Exp Fluids 37(4):577–588
Samimy M, Kim JH, Kastner J, Adamovich I, Utkin Y (2007) Active control of high-speed and high-reynolds-number jets using plasma actuators. J Fluid Mech 578:305–330
Schülein E, Zheltovodov A, Pimonov E, Loginov M (2010) Experimental and numerical modeling of the bow shock interaction with pulse-heated air bubbles. J Aerosp Innovat 2(3):165–187
Singh A, Little J (2016) Active control of a turbulent mixing layer using a pulsed laser and an ns-DBD plasma actuator. AIAA Paper No 2016-0455
Sperber D, Eckel HA, Steimer S, Fasoulas S (2012) Objectives of laser-induced energy deposition for active flow control. Contrib Plasma Phys 52(7):636–643
Starikovskiy A, Limbach C, Miles R (2016) Trajectory control of small rotating projectiles by laser discharges. AIAA Paper 2016-0459 https://doi.org/10.2514/6.2016-0459
Tamba T, Pham HS, Shoda T, Iwakawa A, Sasoh A (2015) Frequency modulation in shock wave-boundary layer interaction by repetitive-pulse laser energy deposition. Phys Fluids 27:091704
Utkin YG, Keshav S, Kim JH, Kastner J, Adamovich IV, Samimy M (2007) Development and use of localized arc filament plasma actuators for high-speed flow control. J Phys D Appl Phys 40:685–694. https://doi.org/10.1088/0022-3727/40/3/S06
Wieneke B (2015) Piv uncertainty quantification from correlation statistics. Measurement Sci Technol 26(7):074002
Winters C, Wagner JL (2019) Interaction of burst-mode laser-induced-plasma with an overexpanded jet at 5–500 kHz repetition-rate. AIAA Paper No 2019-0835
Yan H, Adelgren R, Boguszko M, Elliott G, Knight D (2003a) Laser energy deposition in quiescient air. AIAA J 41(10):1988–1995
Yan H, Adelgren R, Elliott G, Knight D, Beutner T (2003b) Effect of energy addition on MR \(\rightarrow\) RR transition. Shock Waves 13(2):113–121. https://doi.org/10.1007/s00193-003-0198-x
Yanji H, Diankai W, Qian L, Jifei Y (2014) Interaction of single-pulse laser energy with bow shock in hypersonic flow. Chin J Aeronaut 27(2):241–247
Acknowledgements
The authors would like to thank John Petrowski for his efforts in maintaining the SWT facility and for his advice in installing the smoke generator, Paul Pickard for his aid in constructing the wind tunnel models and Professor Doyle D. Knight for providing his expertise on the subject. The authors gratefully acknowledge the Emil Buehler Perpetual Trust for their support of the Buehler Supersonic Wind Tunnel.
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Pournadali Khamseh, A., Kiriakos, R.M. & DeMauro, E.P. Stereoscopic particle image velocimetry of laser energy deposition on a mach 3.4 flow field. Exp Fluids 62, 39 (2021). https://doi.org/10.1007/s00348-021-03142-6
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DOI: https://doi.org/10.1007/s00348-021-03142-6