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Cfd validation experiment of a mach 2.5 axisymmetric shock-wave/boundary-layer interaction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Davis, David O. |
| Copyright Year | 2015 |
| Description | Experimental investigations of specific flow phenomena, e.g., Shock Wave Boundary-Layer Interactions (SWBLI), provide great insight to the flow behavior but often lack the necessary details to be useful as CFD validation experiments. Reasons include: 1.Undefined boundary conditions Inconsistent results 2.Undocumented 3D effects (CL only measurements) 3.Lack of uncertainty analysis While there are a number of good subsonic experimental investigations that are sufficiently documented to be considered test cases for CFD and turbulence model validation, the number of supersonic and hypersonic cases is much less. This was highlighted by Settles and Dodsons [1] comprehensive review of available supersonic and hypersonic experimental studies. In all, several hundred studies were considered for their database.Of these, over a hundred were subjected to rigorous acceptance criteria. Based on their criteria, only 19 (12 supersonic, 7 hypersonic) were considered of sufficient quality to be used for validation purposes. Aeschliman and Oberkampf [2] recognized the need to develop a specific methodology for experimental studies intended specifically for validation purposes. |
| File Size | 4364467 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20150022184 |
| Archival Resource Key | ark:/13960/t76t5p584 |
| Language | English |
| Publisher Date | 2015-07-26 |
| Access Restriction | Open |
| Subject Keyword | Turbulence Modeling Superonic Flow Shock-wave/boundary Layer Interaction Supersonic Flow Turbulent Flow Supersonic Speed Computational Fluid Dynamics Reynolds Number Flow Measurement Shock Wave Interaction Boundary Layers Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
