Volume 3, Issue 2
Hypersonic Limit for Steady Compressible Euler Flows Passing Straight Cones

Qianfeng Li, Aifang Qu, Xueying Su & Hairong Yuan

Commun. Math. Anal. Appl., 3 (2024), pp. 136-167.

Published online: 2024-07

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  • Abstract

We investigate the hypersonic limit for steady, uniform, and compressible polytropic gas passing a symmetric straight cone. By considering Radon measure solutions, we show that as the Mach number of the upstream flow tends to infinity, the measures associated with the weak entropy solution containing an attached shock ahead of the cone converge vaguely to the measures associated with a Radon measure solution to the conical hypersonic-limit flow. This justifies the Newtonian sine-squared pressure law for cones in hypersonic aerodynamics. For Chaplygin gas, assuming that the Mach number of the incoming flow is less than a finite critical value, we demonstrate that the vertex angle of the leading shock is independent of the conical body’s vertex angle and is totally determined by the incoming flow’s Mach number. If the Mach number exceeds the critical value, we explicitly construct a Radon measure solution with a concentration boundary layer.

  • AMS Subject Headings

35L50, 35L65, 35Q31, 35R06, 76K05

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COPYRIGHT: © Global Science Press

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@Article{CMAA-3-136, author = {Li , QianfengQu , AifangSu , Xueying and Yuan , Hairong}, title = {Hypersonic Limit for Steady Compressible Euler Flows Passing Straight Cones}, journal = {Communications in Mathematical Analysis and Applications}, year = {2024}, volume = {3}, number = {2}, pages = {136--167}, abstract = {

We investigate the hypersonic limit for steady, uniform, and compressible polytropic gas passing a symmetric straight cone. By considering Radon measure solutions, we show that as the Mach number of the upstream flow tends to infinity, the measures associated with the weak entropy solution containing an attached shock ahead of the cone converge vaguely to the measures associated with a Radon measure solution to the conical hypersonic-limit flow. This justifies the Newtonian sine-squared pressure law for cones in hypersonic aerodynamics. For Chaplygin gas, assuming that the Mach number of the incoming flow is less than a finite critical value, we demonstrate that the vertex angle of the leading shock is independent of the conical body’s vertex angle and is totally determined by the incoming flow’s Mach number. If the Mach number exceeds the critical value, we explicitly construct a Radon measure solution with a concentration boundary layer.

}, issn = {2790-1939}, doi = {https://doi.org/10.4208/cmaa.2024-0008}, url = {http://global-sci.org/intro/article_detail/cmaa/23226.html} }
TY - JOUR T1 - Hypersonic Limit for Steady Compressible Euler Flows Passing Straight Cones AU - Li , Qianfeng AU - Qu , Aifang AU - Su , Xueying AU - Yuan , Hairong JO - Communications in Mathematical Analysis and Applications VL - 2 SP - 136 EP - 167 PY - 2024 DA - 2024/07 SN - 3 DO - http://doi.org/10.4208/cmaa.2024-0008 UR - https://global-sci.org/intro/article_detail/cmaa/23226.html KW - Compressible Euler equations, shock wave, conical flow, hypersonic limit, Radon measure solution. AB -

We investigate the hypersonic limit for steady, uniform, and compressible polytropic gas passing a symmetric straight cone. By considering Radon measure solutions, we show that as the Mach number of the upstream flow tends to infinity, the measures associated with the weak entropy solution containing an attached shock ahead of the cone converge vaguely to the measures associated with a Radon measure solution to the conical hypersonic-limit flow. This justifies the Newtonian sine-squared pressure law for cones in hypersonic aerodynamics. For Chaplygin gas, assuming that the Mach number of the incoming flow is less than a finite critical value, we demonstrate that the vertex angle of the leading shock is independent of the conical body’s vertex angle and is totally determined by the incoming flow’s Mach number. If the Mach number exceeds the critical value, we explicitly construct a Radon measure solution with a concentration boundary layer.

Li , QianfengQu , AifangSu , Xueying and Yuan , Hairong. (2024). Hypersonic Limit for Steady Compressible Euler Flows Passing Straight Cones. Communications in Mathematical Analysis and Applications. 3 (2). 136-167. doi:10.4208/cmaa.2024-0008
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