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Hartmann Effect. Region of Existence and Oscillation Frequencies

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Abstract

Data of experiments on determining the region of existence for auto‐oscillations (Hartmann effect) with a frequency of approximately 450 Hz with variation in the distance from the nozzle to the resonator. Results of these experiments differ from the well‐known results of Hartmann and his followers obtained for shallow resonators. It is shown that the region of auto‐oscillations exists for large distances between the nozzle and the resonator. The results obtained are explained using the modern knowledge of the gas‐dynamic structure of a supersonic underexpanded jet. It is shown that in determining the frequency of low‐frequency oscillations, it suffices to allow for the resonator length and its “added” mass.

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REFERENCES

  1. Yu. Ya. Borisov, Gas-Jet Oscillators of the Hartmann Type. Sources of Powerful Ultrasound, L. D. Rosenberg (ed.) [in Russian], Nauka, Moscow (1967).

    Google Scholar 

  2. V. G. Dulov and G. A. Luk'yanov, Gasdynamics of Flow Processes [in Russian], Nauka, Novosibirsk (1984).

    Google Scholar 

  3. Tsein Che-Sun, “Axisymmetric supersonic turbulent jet issuing from a nozzle with underexpansion,” in: G. N. Abramovich (ed.), Investigation of Turbulent Air Jets, Plasma, and Real Gas (collected scientific papers) [Russian translation], Mashinostroenie, Moscow (1967).

    Google Scholar 

  4. C. H. Lewis (Jr.) and D. J. Carlson, “Normal shock location in underexpanded gas and gas-particle jets,” AIAA J., 2, No. 4 (1964).

    Google Scholar 

  5. Yu. V. Finat'ev and L. A. Shcherbakov, “On the possibility of approximating the boundaries of an underexpanded axisymmetric jet by an arc of an ellipse,” Inzh.-Fiz. Zh., 17, No. 4, 737–741 (1969).

    Google Scholar 

  6. E. A. Ugryumov, “Gasdynamics of interaction of a supersonic jet with a dead-end channel,” in: V. G. Dulov (ed.), Gas-Dynamics and Acoustics of Jet Flows (collected scientific papers) [in Russian], Inst. Theor. and Appl. Mech., Sib. Div., Acad. of Sci. of the USSR, Novosibirsk (1987), pp. 66–73.

    Google Scholar 

  7. G. V. Naberezhnova and Yu. N. Nesterov, “Unstable interaction of a supersonic underexpanded jet with a cylindrical cavity,” Uch. Zap. TsAGI, 14, No. 5, 58–64 (1983).

    Google Scholar 

  8. V. M. Kuptsov, S. I. Ostroukhova, and K. N. Filippov, “Pressure oscillations and heating of gas with ow of a supersonic jet into a cylindrical cavity,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 5, 104–111 (1977).

  9. V. M. Ustinov, “Experimental investigation of pressure oscillations in a resonant tube,” in: Applied Problems of Hydrogasdynamics (collected scienti_c papers) [in Russian], Regional Pedagog. Inst., Moscow (1986), pp. 52–60.

    Google Scholar 

  10. B. G. Semiletinko and V. N. Uskov, “Experimental dependences for the position of shock waves in a jet incident on an obstacle normal to the jet axis,” Inzh.-Fiz. Zh., 23, No. 3, 453–458 (1972).

    Google Scholar 

  11. A. V. Solotchin, “Experimental investigation of the incidence of a supersonic underexpanded jet on a at obstacle,” Candidate's Dissertation in Tech. Sci., Novosibirsk (1982).

    Google Scholar 

  12. V. N. Glaznev, A. V. Solotchin, and Sh. Suleimanov, “Parametric analysis of auto-oscillations in the case of a supersonic jet owing into a cylindrical cavity,” Izv. Sib. Otd. Aakd. Nauk SSSR, Ser. Tekh. Nauk, No. 13, Issue 3, 22–26 (1983).

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Glaznev, V.N., Korobeinikov, Y.G. Hartmann Effect. Region of Existence and Oscillation Frequencies. Journal of Applied Mechanics and Technical Physics 42, 616–620 (2001). https://doi.org/10.1023/A:1019247529314

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  • DOI: https://doi.org/10.1023/A:1019247529314

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