Projectile thrust-drag optimization with external burning
| dc.contributor.advisor | Fuhs, Allen E. | |
| dc.contributor.author | Smithey, William John Henry | |
| dc.contributor.department | Aeronautics | |
| dc.contributor.school | Naval Postgraduate School | |
| dc.date.accessioned | 2012-11-14T00:00:23Z | |
| dc.date.available | 2012-11-14T00:00:23Z | |
| dc.date.issued | 1974-06 | |
| dc.description.abstract | External burning increases base pressure. The characteristic and linearized equations with heat addition are discuss ed, and the condition for maintaining irrotationa ity with heat addition is derived. A transition model, which extends the Crocco-Lees base flow model, and a spin model are discussed. Computed results are compared with experiment. The optimum location for supersonic external burning is given. | en_US |
| dc.description.distributionstatement | Approved for public release; distribution is unlimited. | |
| dc.description.service | Commander, United States Navy | en_US |
| dc.description.uri | http://archive.org/details/projectilethrust1094517185 | |
| dc.identifier.uri | https://hdl.handle.net/10945/17185 | |
| dc.language.iso | en_US | |
| dc.publisher | Monterey, California. Naval Postgraduate School | en_US |
| dc.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. | en_US |
| dc.subject.lcsh | Aeronautics | en_US |
| dc.title | Projectile thrust-drag optimization with external burning | en_US |
| dc.type | Thesis | en_US |
| dspace.entity.type | Publication | |
| etd.thesisdegree.grantor | Naval Postgraduate School | en_US |
| etd.thesisdegree.level | Doctoral | en_US |
| etd.thesisdegree.name | Ph.D. | en_US |
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