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    Supersonic flow of a Chaplygin gas past a delta wing

    作者: 时间:2025-10-22 浏览次数:

    讲座题目:Supersonic flow of a Chaplygin gas past a delta wing

    主办单位:数理学院/三峡数学研究中心

    报告专家:龙柄菘

    报告时间:2025年11月1日 8:00

    报告地点:L2620

    报告摘要:In this talk, we will present the research progress on the problem of supersonic flow past a delta wing in a Chaplygin gas, including attached and detached shocks to the leading edge. Moreover, we focus on its application in the study of Nonweiler wing, which is a class of the simplest waveriders. Mathematically, this problem can ultimately be reduced to a boundary value problem of a degenerate elliptic equation. Using the intrinsic structure of the equation and the continuity method, we showed that the problem admits a global self-similar solution. Our results verify K\"uchemann's partial speculation on the global conical flow field structures of this type.

    专家简介:龙柄菘,黄冈师范学院讲师,博士毕业于复旦大学。主要研究方向为双曲守恒律方程组的数学理论,包括三角翼超音速绕流问题及其在乘波体理论中的应用、高超音速绕流问题等。主持湖北省自然科学基金项目一项,在Sci. China Math.等期刊上已发表论文6篇。


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