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Laser energy deposition in crossing shock interaction

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Shock Waves

Abstract

A combined computational and experimental study was performed to investigate the effect of a single laser energy pulse on the transition from a Mach Reflection (MR) to a Regular Reflection (RR) in the Dual Solution Domain (DSD). The freestream Mach number is 3.45 and two oblique shock waves are formed by two symmetric 22° wedges. These conditions correspond to a point midway within the DSD wherein either an MR or an RR is possible. A steady MR was first obtained experimentally and numerically, then a single laser pulse was deposited above the horizontal center plane. The experiment showed that the Mach stem height decreased to 30% of its original height due to the interaction with the thermal spot generated by the laser pulse and then returned to its original height by 300μs. That the Mach stem returned to its original height was most likely due to freestream turbulence in the wind tunnel. The numerical simulation successfully predicted the reverse transition from a stable MR to a stable RR and the stable RR persisted across the span. This study showed the capability of a laser energy pulse to control the reverse transition of MR → RR within the Dual Solution Domain.

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References

  1. R. Adelgren, G. Elliott, D. Knight, M. Ivanov: Preliminary study of localized pulsed laser energy deposition effects on shock structures in Mach/regular reflection dual solution domain at Mach 3.45. Report RU-TR-MAE-213, Dept of Mechanical and Aerospace Engineering, Rutgers University, (July 2001)

    Google Scholar 

  2. R. Adelgren: Localized Flow Control with Energy Deposition. Ph.D dissertation, Dept of Mechanical and Aerospace Engineering, Rutgers University, (September 2002)

    Google Scholar 

  3. G. Ben-Dor, M. Ivanov, E.I. Vasilev, T. Elperin: Hysteresis processes in the regular reflection — Mach reflection transition in steady flows. Progress in Aerospace Sciences 38, 347 (2002)

    Article  ADS  Google Scholar 

  4. G.G. Chernity: Some recent results in aerodynamic applications of flows with localized energy addition. AIAA Paper 99-4819 (1999)

    Google Scholar 

  5. A. Chpoun, D. Passerei, J.C. Lengrand, H. Li, G. Ben-Dor: Mise en evidence expérimentale et numérique d’un phénomène d’hysteresis lors de la transition reflexion de Mach-reflexion reguliere. C R Acad Sei Paris 319(2), 1447 (1994)

    Google Scholar 

  6. H. Hornung, H. Oertel, R. Sandeman: Transition to Mach reflection of shock waves in steady and pseudosteady flow with and without relaxation. J. Fluid Mechanics 90, 541 (1979)

    Article  ADS  Google Scholar 

  7. M. Ivanov, S. Gimelshein, A. Beylich: Hysteresis effect in stationary reflection of shock waves. Physics of Fluids 7, 685 (1995)

    Article  ADS  Google Scholar 

  8. M. Ivanov, G. Ben-Dor, T. Elperin, A. Kudryavtsev, D. Khotyanovsky: The reflection of asymmetric shock waves in steady flows: A numerical investigation. Journal of Fluid Mech. 469, 71 (2002)

    Article  ADS  MathSciNet  Google Scholar 

  9. V. Levin, L. Terent’eva: Supersonic flow over a cone with heat release in the neighborhood of the apex. Mekhanika Zhidkosti i Gaza 2, 110 (1993)

    Google Scholar 

  10. H. Li, A. Chpoun, G. Ben-Dor: Analytical and experimental investigation of the reflection of asymmetric shock waves in steady flows. Journal of Fluid Mech. 390, 25 (1999)

    Article  ADS  MathSciNet  Google Scholar 

  11. D. Riggins, H. Nelson, E. Johnson: Blunt body wave drag reduction using focused energy deposition. AIAA J. 37(4), 460 (1999)

    Article  ADS  Google Scholar 

  12. P. Toro, L. Myrabo, H. Nagamatsu: Pressure investigation of the hypersonic ‘Directed Energy Air Spike’ inlet at Mach number 10 up to 70kW. AIAA Paper 98-0991 (1998)

    Google Scholar 

  13. J. Von Neumann: in Collected Works, Pergamon Press 6, 239 (1963)

    Google Scholar 

  14. H. Yan, R. Adelgren, M. Boguszko, G. Elliott, D. Knight: Laser energy deposition in quiescent air. AIAA Paper 2003-1051 (2003)

    Google Scholar 

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© 2005 Tsinghua University Press and Springer-Verlag Berlin Heidelberg

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Yan, H., Knight, D., Elliott, G. (2005). Laser energy deposition in crossing shock interaction. In: Jiang, Z. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_81

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  • DOI: https://doi.org/10.1007/978-3-540-27009-6_81

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-22497-6

  • Online ISBN: 978-3-540-27009-6

  • eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)

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