Abstract
The considered sequential approximation method for one-dimensional unsteady problems makes it possible to reduce the solution to the integration of systems of ordinary differential equations. The gas motion is bounded, on the one hand, by a piston moving in accordance with an arbitrary law, and, on the other hand, by either a compression shock or a rarefaction wave propagating through the gas with given arbitrary parameters. A comparison is made of certain exact solutions with the resulting approximate solutions.
Similar content being viewed by others
References
N. Kotchine, Rendiconti del Circolo Mat, de Palermo, 50, 1926.
L. I. Sedov, Similarity and Dimensional Methods in Mechanics [in Russian], 5th edition, Izd-vo Nauka, 1965.
L. D. Landau and E. M. Lifshitz, Mechanics of Continuous Media [in Russian], 2nd edition, Gostekhlzdat, 1954.
Ya. B. Zel'dovich and Yu. P. Raizer, Physics of Shock Waves and High-Temperature Hydrodynamic Phenomena [in Russian], chapter 12, 15, 22, 23, Fizmatgiz, 1963,
D. E. Okhotsimskii, I. A. Kondrasheva, Z. P. Vlasov, and R. K. Kazakova, “Calculation of a point blast with account for the counterpressure,” Tr. Matem. in-ta AN SSSR, vol. 50, 1957.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Andreev, V.P. Sequential approximation method for one-dimensional unsteady problems of gasdynamics. Fluid Dyn 2, 19–22 (1967). https://doi.org/10.1007/BF01013706
Issue Date:
DOI: https://doi.org/10.1007/BF01013706