Infrared and Laser Engineering, Volume. 48, Issue 4, 406001(2019)

Influence of key parameters on the interaction of the laser induced plasma hot core and shock wave

Wen Ming, Wang Diankai, and Wang Weidong
Author Affiliations
  • [in Chinese]
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    References(14)

    [1] [1] Kremeyer K, Sebastian K, Shu C W. Computational study of shock mitigation and drag reduction by pulsed energy lines[J]. AIAA Journal, 2006, 44(8): 1720-1731.

    [2] [2] Guvernyuk S V, Samoilov A B. Control of supersonic flow around bodies by means of a pulsed heat source[J]. Tech Phys Lett, 1997, 23(5): 333-336.

    [3] [3] Oliveira C, Minucci M A, Toro P G, et al. Bow shock wave mitigation by laser-plasma energy addition in hypersonic flow[J]. Journal of Spacecraft and Rockets, 2008, 45(5): 921-927.

    [4] [4] Hong Junwu, Chen Xiaodong, Zhang Yulun, et al. The primary numerical research of active control technology in flow[J]. Acta Aerodynamica Sinica, 2005, 23(4): 402-407. (in Chinese)

    [5] [5] Minucci M A S, Chanes J B, Myrabo L N, et al. Investigation of a laser-supported directed-energy "air spike" in hypersonic flow[J]. Journal of Spacecraft and Rockets, 2003, 40(1): 133-136.

    [6] [6] Oliveira A C, Minucci M A S, Toro P G P, et al. Schlieren visualization technique applied to the study of laser-induced breakdown in low density hypersonic Flow[C]//Beamed Energy Propulsion: Fourth International Symposium on Beamed Energy Propulsion, AIP Publishing, 2006, 830(1): 504-509.

    [7] [7] Oliveira A C, Minucci M A, Myrabo L N, et al. Bow shock wave mitigation by laser-plasma energy addition in hypersonic flow[J]. Journal of Spacecraft and Rockets, 2008, 45(5): 921-927.

    [8] [8] Sasoh A, Kim J H, Yamashita K, et al. Fly by light power: improvement of supersonic aerodynamic performance with high-repetitive-rate energy depositions: examination of truncated cones[R]. AIAA Paper, 2011-3999, 2011.

    [9] [9] Schülein E, Zheltovodov A A, Pimonov E A, et al. Study of the bow shock interaction with laser-pulse-heated air bubbles[R]. AIAA Paper, 2009-3568, 2009.

    [10] [10] Ogino Y, Ohnishi N, Taguchi S, et al. Baroclinic vortex influence on wave drag reduction induced by pulse energy deposition[J]. Physics of Fluids, 2009, 21(6): 0661021.

    [11] [11] Niederhaus J, Greenough A, Oakley G, et al. Computational parameter study for the three-dimensional shock-bubble interaction[J]. Journal of Fluid Mechanics, 2008, 594: 85-124.

    [12] [12] Sasoh A, Sekiya Y, Sakai T, et al. Supersonic drag reduction with repetitive laser pulses through a blunt body[R]. AIAA Paper, 2009-3585, 2009.

    [13] [13] Azarova O A. Supersonic flow control using combined energy deposition[J]. Aerospace, 2015, 2(1): 118-134.

    [14] [14] Zel′dovich Y B, Raizer Y P. Physics of Shock Waves and High-Temperature Hydrodynamic Phenomena[M]. Mineola, New York: Dover Publications, Inc, 2002.

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    Wen Ming, Wang Diankai, Wang Weidong. Influence of key parameters on the interaction of the laser induced plasma hot core and shock wave[J]. Infrared and Laser Engineering, 2019, 48(4): 406001

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    Paper Information

    Received: Nov. 22, 2018

    Accepted: Dec. 16, 2018

    Published Online: Jul. 23, 2019

    The Author Email:

    DOI:10.3788/irla201948.0406001

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