Outline of a Theory of non-Rankine-Hugoniot Shock Wave in Weak Mach Reflection
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At the previous AFMC, the background for expecting a departure from Rankine-Hugoniot theory at the base of the reflected shock wave in weak Mach reflection was exposed. The results of some pertinent experiments performed in the supersonic wind tunnel were then presented. They confirmed the hypothesised irregular behaviour. In the present contribution, the elaboration of a theory of transgressed shock wave properties is presented. This concept enables to calculate the modified jump process. It fully accounts for the known experimental observations. It is the unyielding boundary conditions that prevail beyond regular reflection which force this remarkable deviation from the classical shock wave theory to take place.
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| ID Code: | 2640 |
|---|---|
| Item Type: | Contribution to conference (Paper/Presentation) |
| Refereed: | No |
| Pure ID: | 57187510 |
| Divisions: | Past > QUT Faculties & Divisions > Faculty of Built Environment and Engineering Current > Research Centres > Australian Research Centre for Aerospace Automation |
| Copyright Owner: | Copyright 2001 (please consult author) |
| Copyright Statement: | This work is covered by copyright. Unless the document is being made available under a Creative Commons Licence, you must assume that re-use is limited to personal use and that permission from the copyright owner must be obtained for all other uses. If the document is available under a Creative Commons License (or other specified license) then refer to the Licence for details of permitted re-use. It is a condition of access that users recognise and abide by the legal requirements associated with these rights. If you believe that this work infringes copyright please provide details by email to qut.copyright@qut.edu.au |
| Deposited On: | 21 Nov 2005 00:00 |
| Last Modified: | 03 Mar 2024 09:01 |
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