In this paper, we establish the first rigorous mathematical result on the validation of the hypersonic similarity globally, which is also called the Mach-number independence principle, for the two dimensional steady potential flow. The hypersonic similarity is equivalent to the Van Dyke's similarity theory, that is, if the hypersonic similarity parameter K is fixed, the shock solution structures (after scaling) are consistent, when the Mach number of the flow is sufficiently large. One of the difficulty is that after scaling, the solutions are usually of large data since the perturbation of the hypersonic flow is usually not small related to the sonic speed. In order to make it, we first develop a modified Glimm scheme to construct the approximate solutions with large data and find fine structure of the elementary wave curves to obtain the global existence of entropy solutions with large data, for fixed K and sufficiently large Mach number of the incoming flow . Finally, we further show that for a fixed hypersonic similarity parameter K, if the Mach number , the solutions obtained above approach to the solution of the corresponding initial-boundary value problem of the hypersonic small-disturbance equations. Therefore, the Van Dyke's similarity theory is verified rigorously for the first time.
Mots-clés : Hypersonic similarity, Steady potential flow, Hypersonic flow, Glimm scheme, BV solutions with large data
@article{AIHPC_2020__37_6_1379_0, author = {Kuang, Jie and Xiang, Wei and Zhang, Yongqian}, title = {Hypersonic similarity for the two dimensional steady potential flow with large data}, journal = {Annales de l'I.H.P. Analyse non lin\'eaire}, pages = {1379--1423}, publisher = {Elsevier}, volume = {37}, number = {6}, year = {2020}, doi = {10.1016/j.anihpc.2020.05.002}, mrnumber = {4168920}, zbl = {1456.35138}, language = {en}, url = {http://archive.numdam.org/articles/10.1016/j.anihpc.2020.05.002/} }
TY - JOUR AU - Kuang, Jie AU - Xiang, Wei AU - Zhang, Yongqian TI - Hypersonic similarity for the two dimensional steady potential flow with large data JO - Annales de l'I.H.P. Analyse non linéaire PY - 2020 SP - 1379 EP - 1423 VL - 37 IS - 6 PB - Elsevier UR - http://archive.numdam.org/articles/10.1016/j.anihpc.2020.05.002/ DO - 10.1016/j.anihpc.2020.05.002 LA - en ID - AIHPC_2020__37_6_1379_0 ER -
%0 Journal Article %A Kuang, Jie %A Xiang, Wei %A Zhang, Yongqian %T Hypersonic similarity for the two dimensional steady potential flow with large data %J Annales de l'I.H.P. Analyse non linéaire %D 2020 %P 1379-1423 %V 37 %N 6 %I Elsevier %U http://archive.numdam.org/articles/10.1016/j.anihpc.2020.05.002/ %R 10.1016/j.anihpc.2020.05.002 %G en %F AIHPC_2020__37_6_1379_0
Kuang, Jie; Xiang, Wei; Zhang, Yongqian. Hypersonic similarity for the two dimensional steady potential flow with large data. Annales de l'I.H.P. Analyse non linéaire, Tome 37 (2020) no. 6, pp. 1379-1423. doi : 10.1016/j.anihpc.2020.05.002. http://archive.numdam.org/articles/10.1016/j.anihpc.2020.05.002/
[1] Wave-front tracking for the equations of isentropic gas dynamics, Q. Appl. Math., Volume 63 (2005), pp. 20–33 | MR | Zbl
[2] Wave-front tracking for the equations of non-isentropic gas dynamics, Ann. Math., Volume 194 (2015), pp. 581–618 | MR | Zbl
[3] Hypersonic and High-Temperature Gas Dynamics, AIAA Education Series, Reston, 2006
[4] Hyperbolic Systems of Conservation Laws. The One-Dimensional Cauchy Problem, Oxford University Press, Oxford, 2000 | DOI | MR | Zbl
[5] Continuous dependence of entropy solutions to the Euler equations on the adiabatic exponent and Mach number, Arch. Ration. Mech. Anal., Volume 189 (2008), pp. 97–130 | MR | Zbl
[6] Well-posedness of transonic characteristic discontinuities in two-dimensional steady compressible Euler flows, Z. Angew. Math. Phys., Volume 64 (2013), pp. 1711–1727 | MR | Zbl
[7] Two-dimensional steady supersonic exothermically reacting Euler flow past Lipschitz bending walls, SIAM J. Math. Anal., Volume 49 (2017), pp. 818–873 | MR | Zbl
[8] Well-posedness for two-dimensional steady supersonic Euler flows past a Lipschitz wedge, J. Differ. Equ., Volume 244 (2008), pp. 1521–1550 | MR | Zbl
[9] Weakly nonlinear geometric optics for hyperbolic systems of conservation laws, Commun. Partial Differ. Equ., Volume 38 (2015), pp. 1936–1970 | MR | Zbl
[10] Existence and stability of supersonic Euler flows past Lipschitz wedges, Arch. Ration. Mech. Anal., Volume 181 (2006), pp. 261–310 | MR | Zbl
[11] A Study of Hypersonic Small Disturbance Theory, 1954 (NACA Rept., 1194, April) | MR
[12] Solutions in the large for nonlinear hyperbolic systems of equations, Commun. Pure Appl. Math., Volume 18 (1965), pp. 697–715 | DOI | MR | Zbl
[13] Stability of transonic jet with strong shock in two-dimensional steady compressible Euler flows, J. Differ. Equ., Volume 258 (2015), pp. 2572–2617 | DOI | MR | Zbl
[14] Fluid Mechanics, Elsevier Ltd., Singapore, 2004
[15] Solutions in the large for the equations of nonisentropic, Indiana Univ. Math., Volume 26 (1977), pp. 147–177 | MR | Zbl
[16] Global solution for an initial-boundary value problem of a quasilinear hyperbolic system, Proc. Jpn. Acad., Volume 44 (1968), pp. 642–646 | MR | Zbl
[17] Solutions in the large for some nonlinear hyperbolic conservation laws, Commun. Pure Appl. Math., Volume 26 (1973), pp. 183–200 | DOI | MR | Zbl
[18] Mixed problems for nonlinear conservation laws, J. Differ. Equ., Volume 23 (1977), pp. 244–269 | DOI | MR | Zbl
[19] Hypersonic limit of two-dimensional steady compressible Euler flows passing a straight wedge, Z. Angew. Math. Mech. (2020) | DOI | MR | Zbl
[20] Similarity laws of hypersonic flows, J. Math. Phys., Volume 25 (1946), pp. 247–251 | MR | Zbl
[21] Shock Waves and Reaction-Diffusion Equations, Springer-Verlag, Inc., New York, 1994 | MR | Zbl
[22] Solutions in the large for the nonlinear hyperbolic conservation laws of gas dynamics, J. Differ. Equ., Volume 41 (1981), pp. 96–161 | DOI | MR | Zbl
[23] Two-dimensional steady supersonic exothermically reacting Euler flows with strong contact discontinuity over Lipschitz wall, Interfaces Free Bound., Volume 20 (2018), pp. 437–481 | DOI | MR | Zbl
[24] Global existence of steady supersonic potential flow past a curved wedge with piecewise smooth boundary, SIAM J. Math. Anal., Volume 31 (1999), pp. 166–183 | DOI | MR | Zbl
[25] Steady supersonic flow past an almost straight wedge with large vertex angle, J. Differ. Equ., Volume 192 (2003), pp. 1–46 | DOI | MR | Zbl
Cité par Sources :