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Experimental investigation of gasdynamic processes at sudden start-up of a supersonic nozzle

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Literature cited

  1. V. N. Kroshko, R. I. Soloukhin and N. A. Fomin, “Gasdynamic processes in generating inversions in shock tubes,” Fiz. Goreniya Vzryva, No. 3 (1973).

  2. C. E. Smith, “An analytical study of the starting process in a hypersonic nozzle,” in: Proc. Heat Transfer and Fluid Mech. Inst., Stanford University Press (1964), p. 198.

  3. R. M. Marmey and J. P. Guibergia, “Etude experimental des phenomenes accompagnant l'amorgage d'une fuére hypersonique,” C. R., Ser. AB,271, No. 2, 106 (1970).

    Google Scholar 

  4. C. E. Smith, “The starting process in a hypersonic nozzle,” J. Fluid Mech.,24, Part 4 (1966).

  5. J. A. Ackroyd, “A study of test time in reflected shock tunnels,” ARC CP, No. 883 (1967).

  6. T. Ikui and K. Matsuo, “Investigation of the aerodynamic characteristics of the shock tube,” Bull. JSME, 15, No. 82 (1972).

    Google Scholar 

  7. M. Dawn, “Experimental investigation of high enthalpy flow in a shock tube,” Raket. Tekh. Kosmon., No. 8, 9 (1969).

    Google Scholar 

  8. A. K. Oppenheim, P. A. Urtiew and A. J. Landerman, “Vector polar method for the evaluation of wave interaction processes,” Arch. Budowy Masz.,11, No. 3 (1964).

  9. H. O. Amann, “Experimental study of the starting process in a reflected nozzle,” Phys. Fluids, Suppl. 1 (1969).

  10. H. O. Amann, “Vorgänge beim Start einer ebener Reflexiondüse,” Z. Flügwiss.,19, 393 (1971).

    Google Scholar 

  11. G. M. Rudakova and A. P. Shashkin, “Computation of some two-dimensional unsteady gas flows,” Izv. Sib. Otd. Akad. Nauk SSSR, Ser. Tekh. Nauk, No. 3, Issue 1, 70 (1975).

    Google Scholar 

  12. R. F. Chisnell, “The motion of a shock wave in a channel, with application to cylindrical and spherical shock waves,” J. Fluid Mech.,2 (1957).

  13. L. Bernstein, “Equilibrium real-gas performance charts for a hypersonic shock-tube wind-tunnel employing nitrogen,” ARC CP, No. 633 (1961).

  14. R. A. Alpher and D. R. White, “Flow in shock tubes with area change at the diaphragm section,” J. Fluid Mech.,3, 457 (1958).

    Google Scholar 

  15. W. Chester, “The diffraction and reflection of shock waves,” J. Mech. Appl. Math.,7, Part 1, 57 (1954).

    Google Scholar 

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Authors and Affiliations

  1. Moscow

    L. G. Gvozdeva & Yu. V. Zhilin

Authors
  1. L. G. Gvozdeva
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  2. Yu. V. Zhilin
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Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 4, pp. 66–74, July–August, 1977.

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Gvozdeva, L.G., Zhilin, Y.V. Experimental investigation of gasdynamic processes at sudden start-up of a supersonic nozzle. J Appl Mech Tech Phys 18, 484–491 (1977). https://doi.org/10.1007/BF00851389

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  • DOI: https://doi.org/10.1007/BF00851389

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