@Article{CMAA-3-2,
author = {Zhang, Yongqian},
title = {A Local Inverse Conical Shock Problem for the Steady Supersonic Potential Flow},
journal = {Communications in Mathematical Analysis and Applications},
year = {2024},
volume = {3},
number = {2},
pages = {287--313},
abstract = {<p style="text-align: justify;">This paper studies an inverse problem of reconstructing the shape of
the circular symmetric cone for the given leading shock front. Assuming that
the attack angle is small and that the incoming flow has a large Mach Number, we show that the shape of the cone can be reconstructed near the vertex
from the data of the given shock and establish an asymptotic expansion for the
velocity and the slope of cone.</p>},
issn = {2790-1939},
doi = {https://doi.org/10.4208/cmaa.2024-0012},
url = {https://global-sci.com/article/90969/a-local-inverse-conical-shock-problem-for-the-steady-supersonic-potential-flow}
}