Abstract
The transient regime in gas flow past a stepwise accelerated body is analyzed by the method of singular perturbations at small Froude numbers. A marked effect of the initial conditions on the shock layer gas flow is demonstrated. The problem of flow past a wedge is solved in quadratures.
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References
B. M. Bulakh, “On the motion of a wedge with a variable supersonic velocity through quiescent gas,”Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 113 (1980).
A. B. Vasil’eva and V. F. Butuzov,Asymptotic Expansions of the Solutions of Singularly Perturbed Equations [in Russian], Nauka, Moscow (1973).
3. A. B. Vasil’eva and V. F. Butuzov, “On some results of the theory of singular perturbations obtained in the last five years,”Vestnik MGU, Series 15, Vychisl. Mat. Kib., No. 3, 25 (1981).
Additional information
St.Petersburg. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 1, pp. 111–121, January–February, 1997.
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Bogatko, V.I., Kolton, G.A. On the transient regime in nonstationary supersonic flow past a body. Fluid Dyn 32, 92–102 (1997). https://doi.org/10.1007/BF02697942
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DOI: https://doi.org/10.1007/BF02697942