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Front separation regions for blunt and streamlined bodies initiated by temperature wake – bow shock wave interaction

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Shock Waves

Summary

Front separation flows supported by an upstream energy deposition are examined. It is shown that a reason for separation region formation is an interaction of a thin high temperature wake (“thermal spike”) which is formed downstream a localized energy deposition region with a shock layer upstream of a body. Some simplified analytical models are applied to describe a front separation phenomenon. To realize steady flows with isobaric front separation regions in numerical experiments the “method of transformation of energy deposition” is proposed. The method is applied for both blunt as well as streamlined “thermal spiked” bodies to realize conical front separation regions. “Shock-free” separation flows initiated by subsonic “thermal spikes” are particularly examined.

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References

  1. Georgievsky P., Levin V. : Supersonic Flow over Bodies in the Presence of External Energy Input. Letters to Journal of Technical Physics (in Russian), vol. 14, no. 8, 1988.

    Google Scholar 

  2. Borzov V., Rybka I., Yuriev A. : The Estimation for Power Input Using for Wave Drag Reduction of a Body in a Supersonic Flow. Journal of Engineering and Physics (in Russian), vol. 63, no. 6, 1992.

    Google Scholar 

  3. Tretiyakov P., Grachev G., Ivanchenko A. et al. : Stabilization of an Optical Discharge in a Supersonic Flow of Argon. Proceedings of Russian Academy of Sciences (in Russian), vol. 336, no. 4, 1994.

    Google Scholar 

  4. Artem’ev V., Bergel’son V., Nemchinov I., Orlova T., Smirnov V., Khazins V. : Change of Regime in Supersonic Flow past an Obstacle Preceded by a Thin Channel of Reduced Density. Fluid Dynamics (Historical Archive), vol. 24, no. 5, 1989.

    Google Scholar 

  5. Guvernjuk S., Savinov K. : Shock Layer Structure for the Barrier in the Wake-type Nonuniform Supersonic Flow (in Russian). Institute for Mechanics of Moscow State University , Paper no. 4047, 1990.

    Google Scholar 

  6. Georgievskii P., Levin V. : Control of the Flow past Bodies Using Localized Energy Addition to the Supersonic Oncoming Flow. Fluid Dynamics, vol. 38, no. 5, 2003.

    Google Scholar 

  7. Georgievsky P., Levin V. : Bow Shock Wave Structures Control by Pulse-Periodic Energy Input. AIAA Paper 2004-1019, 2004.

    Google Scholar 

  8. Zheltovodov A. : Development of the Studies on Energy Deposition for Application to the Problems of Supersonic Aerodynamics. Institute of Theoretical and Applied Mechanics, Russian Academy of Sciences, Preprint no. 10-2002, Novosibirsk, Russia, 2002.

    Google Scholar 

  9. Knight D., Yan H., Candler G., Kandala R., Elliot G., Glumac N., Zheltovodov A., Pimonov E. : High Speed Flow Control Using Pulsed Energy Deposition. Proceedings of European Conference for Aerospace Sciences (EUCASS), Moscow, Russia, July 4-7, 2005.

    Google Scholar 

  10. MacCormack R. : The Effect of Viscosity in Hypervelocity mpact Cratering. AIAA Paper 1969-354, 1969.

    Google Scholar 

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© 2009 Springer-Verlag Berlin Heidelberg

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Georgievskiy, P., Levin, V. (2009). Front separation regions for blunt and streamlined bodies initiated by temperature wake – bow shock wave interaction. In: Hannemann, K., Seiler, F. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_77

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  • DOI: https://doi.org/10.1007/978-3-540-85181-3_77

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-85180-6

  • Online ISBN: 978-3-540-85181-3

  • eBook Packages: EngineeringEngineering (R0)

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