Approved for public release; distribution is unlimited / A computer model of the Coanda Refraction Jet Engine Test Cell facility was developed
using the PHOENICS computer code. The PIIOENICS code was utilized to
determine the steady state aerothermal characteristics of the test cell during the testing
of an E404 gas turbine engine with afterburner in operation. Computer generated
aerothermodynamic field variables of pressure, velocity and temperature parameters
were compared to operational field test data. Observations regarding compared results
as well as system behavior are presented. Additionally, recommendations of the applications
of PHOENICS to future modeling projects are made. / http://archive.org/details/aerothermodynami00mara / Lieutenant, United States Navy
| Identifer | oai:union.ndltd.org:nps.edu/oai:calhoun.nps.edu:10945/22863 |
| Date | 12 1900 |
| Creators | Maraoui, André |
| Contributors | Salinas, David, Naval Postgraduate School (U.S.), Mechanical Engineering |
| Publisher | Monterey, California. Naval Postgraduate School |
| Source Sets | Naval Postgraduate School |
| Language | en_US |
| Detected Language | English |
| Type | Thesis |
| Format | 132 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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