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Prandtl-Meyer reflection configurations, transonic shocks, and free boundary problems

Abstract:

We are concerned with the Prandtl-Meyer reflection configurations of unsteady global solutions for supersonic flow impinging upon a symmetric solid wedge. Prandtl (1936) first employed the shock polar analysis to show that there are two possible steady configurations: the steady weak shock solution and the strong shock solution, when a steady supersonic flow impinges upon the solid wedge — the half-angle of which is less than a critical angle (i.e., the detachment angle), and then conjectured...

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Publication status:
Accepted
Peer review status:
Peer reviewed

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Institution:
University of Oxford
Division:
MPLS
Department:
Mathematical Institute
Role:
Author
ORCID:
0000-0001-5146-3839
Publisher:
American Mathematical Society Publisher's website
Series:
Memoirs of the American Mathematical Society
Place of publication:
Providence, RI, USA
EISSN:
1947-6221
ISSN:
0065-9266
Language:
English
Pubs id:
1136264
Local pid:
pubs:1136264
Deposit date:
2020-10-06

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