Approved for public release; distribution is unlimited / Cebeci's viscous/inviscid interaction program was applied
to the analysis of steady, two dimensional, incompressible
flow past four airfoils, the NACA 66₃-018, 0010 (Modified),
4412 and the Wortmann FX 63-137. Detailed comparisons with
the available experimental results show that the essential
features are correctly modelled, but that significant
discrepancies are found in regions of flow separations. / http://archive.org/details/computationalinv00math / Lieutenant, United States Navy
| Identifer | oai:union.ndltd.org:nps.edu/oai:calhoun.nps.edu:10945/22965 |
| Date | 12 1900 |
| Creators | Mathre, John Mark |
| Contributors | Platzer, Max F., Howard, R.M., Naval Postgraduate School (U.S.), Aeronautics and Astronautics |
| Publisher | Monterey, California. Naval Postgraduate School |
| Source Sets | Naval Postgraduate School |
| Language | en_US |
| Detected Language | English |
| Type | Thesis |
| Format | 143 p., application/pdf |
| Rights | This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States. |
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