Second integral generalization of the Crocco invariant for 3D flows behind detached bow shock wave
- Authors: Sizykh G.1
-
Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 25, No 3 (2021)
- Pages: 588-595
- Section: Short Communications
- URL: https://bakhtiniada.ru/1991-8615/article/view/70810
- DOI: https://doi.org/10.14498/vsgtu1861
- ID: 70810
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Abstract
Stationary flows of an ideal gas behind the detached bow shock are investigated in the general 3D case. The well-known integral invariant (V.N. Golubkin, G.B. Sizykh, 2019), generalizing the axisymmetric invariant of (L. Crocco, 1937) to asymmetric flows, is a curvilinear integral over a closed vortex line (such lines lie on isentropic surfaces), in which the integrand is the pressure divided by the vorticity. This integral takes on the same value on all (closed) vortex lines lying on one isentropic surface. It was obtained after the discovery of the fact that the vortex lines are closed in the flow behind the shock in the general 3D case. Recently, another family of closed lines behind the shock was found, lying on isentropic surfaces (G.B. Sizykh, 2020). It is given by vector lines a — the vector product of the gas velocity and the gradient of the entropy function. In the general 3D case, these lines and vortex lines do not coincide.
In the presented study, an attempt is made to find the integral invariant associated with closed vector lines a. Without using asymptotic, numerical and other approximate methods, the Euler equations are analyzed for the classical model of the flow of an ideal perfect gas with constant heat capacities. The concept of imaginary particles “carrying” the streamlines of a real gas flow, based on the Helmholtz–Zoravsky criterion, is used. A new integral invariant of isentropic surfaces is obtained. It is shown that the curvilinear integral over a closed vector line a, in which the integrand is the pressure divided by the projection of the vorticity on the direction a, has the same values for all lines a lying on one isentropic surface. This invariant, like another previously known integral invariant (V.N. Golubkin, G.B. Sizykh, 2019), in the particular case of non-swirling axisymmetric flows, coincides with the non-integral invariant of L. Crocco and generalizes it to the general spatial case.
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##article.viewOnOriginalSite##About the authors
Grigory Sizykh
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: o1o2o3@yandex.ru
ORCID iD: 0000-0001-5821-8596
SPIN-code: 5348-6492
Scopus Author ID: 6508163390
ResearcherId: ABI-3162-2020
http://www.mathnet.ru/person112378
Cand. Phys. & Math. Sci; Associate Professor; Dept. of Applied Mathematics
4, Volokolamskoe shosse, Moscow, 125993, Russian FederationReferences
- Golubkin V. N., Sizykh G. B. On the vorticity behind 3-D detached bow shock wave, Adv. Aerodyn., 2019, vol. 1, 15. https://doi.org/10.1186/s42774-019-0016-5
- Crocco L. Eine neue Stromfunktion für die Erforschung der Bewegung der Gase mit Rotation [A new stream function for researching the movement of gases with rotation], ZAMM, 1937, vol. 17, no. 1, pp. 1–7 (In German). https://doi.org/10.1002/ZAMM.19370170103
- Golubkin V. N., Manuylovich I. S., Markov V. V. Fifth streamline invariant to axisymmetric swirling gas flows, Proceedings of MIPT, 2018, vol. 10, no. 2, pp. 131–135 (In Russian).
- Golubkin V. N., Sizykh G. B. Generalization of the Crocco invariant for 3D gas flows behind detached bow shock wave, Russian Math. (Iz. VUZ), 2019, vol. 63, no. 12, pp. 45–48. https://doi.org/10.3103/S1066369X19120053
- Sizykh G. B. System of Orthogonal Curvilinear Coordinates on the Isentropic Surface Behind a Detached Bow Shock Wave, Fluid Dyn., 2020, vol. 55, no. 7, pp. 899–903. https://doi.org/10.1134/s0015462820070095
- von Mises R. Mathematical Theory of Compressible Fluid Flow, Applied Mathematics and Mechanics, vol. 3. New York, Academic Press, 1958, vii+514 pp. https://doi.org/10.1016/b978-0-123-95621-7.x5001-x
- Prim R., Truesdell C. A derivation of Zorawski’s criterion for permanent vector-lines, Proc. Amer. Math. Soc., 1950, vol. 1, no. 1, pp. 32–34. https://doi.org/10.1090/S0002-9939-1950-0035136-9
- Truesdell C. The Kinematics of Vorticity. Bloomington, IU Press, 1954, xx+232 pp.
- Sizykh G. B. Entropy Value on the Surface of a Non-symmetric Convex Bow Part of a Body in the Supersonic Flow, Fluid Dyn., 2019, vol. 54, no. 7, pp. 907–911. https://doi.org/10.1134/S0015462819070139
- Mironyuk I. Yu., Usov L. A. The invariant of stagnation streamline for a stationary vortex flow of an ideal incompressible fluid around a body, Vestn. Samar. Gos. Tekhn. Univ., Ser. Fiz.-Mat. Nauki [J. Samara State Tech. Univ., Ser. Phys. Math. Sci.], 2020, vol. 24, no. 4, pp. 780–789 (In Russian). https://doi.org/10.14498/vsgtu1815
- Mironyuk I. Yu., Usov L. A. Stagnation points on vortex lines in flows of an ideal gas, Proceedings of MIPT, 2020, vol. 12, no. 4, pp. 171–176 (In Russian).
- Pontryagin L. S. Obyknovennye differentsial’nye uravneniia [Ordinary Differential Equations]. Izhevsk, Regular and Chaotic Dynamics, 2001, 400 pp. (In Russian)
- Truesdell C. On curved shocks in steady plane flow of an ideal fluid, J. Aeronaut. Sci., 1952, vol. 19, no. 12, pp. 826–828. https://doi.org/10.2514/8.2495
- Hayes W. D. The vorticity jump across a gasdynamic discontinuity, J. Fluid Mech., 1957, no. 2, pp. 595–600. https://doi.org/10.1017s0022112057000403
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