Abstract
Results of experimental studies of the unsteady flow around models of a stream moving behind the front of a very strong shock wave excited in an electromagnetic shock tube are presented. The flow establishment time in the stagnation-point region of blunt bodies is found.
Similar content being viewed by others
References
A. S. Dubovik, Photographic Recording of High-Speed Processes [in Russian], 1964.
V. N. Gusev and M. D. Ladyzhenskii, “Gasdynamic design of shock tubes and hypersonic nozzles with equilibrium dissociation and ionization of air,” Tr. TsAGI, no. 779, 1960.
A. S. Predvoditelev, E. V. Stupochenko, et al., Tables of Thermodynamic Functions for Air (at Temperatures from 12 000 to 20 000° K and Pressures from 0.01 to 1000 Atmospheres) [in Russian], Izd-vo AN SSSR, 1959.
K. M. Magomedov, “Supersonic flow about bodies with a known sonic point,” Izv. AN SSSR, OTN, Mekhanika i mashinostroenie, no. 1, 1963.
H. Serbin “Supersonic flow around blunt bodies,” Aeronaut. Sci., vol. 25, no. 1, 1958.
F. G. Shugaev, “Interaction of a supersonic stream with an obstacle,” PMTF, no. 6, 1963.
M. D. Ladyzhenskii and L. G. Chernikova, “Study of shock-wave propagation in a discharge tube,” PMTF, no. 2, 1961.
Alphonso Ambroio and Andrzej Wortman “Stagnation-point shock detachment distance for flow around spheres and cylinders in air,” J. Aerospace Sci., vol. 29, no. 7, 1962.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Bogoslovskii, K.E., Kireeva, N.I., Makarevich, G.A. et al. Unsteady flow around models in an electromagnetic shock tube. Fluid Dyn 1, 71–75 (1966). https://doi.org/10.1007/BF01013819
Issue Date:
DOI: https://doi.org/10.1007/BF01013819