Approved for public release, distribution unlimited / ry at simulated flight conditions, including supersonic cruising conditions. The spiral lines initiator demonstrated a lower total pressure loss with compared to the geometry with rings, and thus was the preferred initiator configuraiton. Experimental values for the turbulence were found to be significantly lower than the computed values at similar conditions when using the k-e model. Finally, successful ignitions of the JP-10/Air initiator at frequencies of up to 20 Hz were experimentally demonstrated. / Funded by: N0001406WR20161.
| Identifer | oai:union.ndltd.org:nps.edu/oai:calhoun.nps.edu:10945/2445 |
| Date | 12 1900 |
| Creators | Hutcheson, Patrick D. |
| Contributors | Brophy, Christopher M., Hobson, Garth V., Naval Postgraduate School (U.S.)., Department of Mechanical |
| Publisher | Monterey California. Naval Postgraduate School |
| Source Sets | Naval Postgraduate School |
| Detected Language | English |
| Type | Thesis |
| Format | xvi, 99 p. : ill. ;, application/pdf |
| Rights | Approved for public release, distribution unlimited, This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted. |
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