{"id":{"repo_id":"nps","oai_identifier":"oai:calhoun.nps.edu:10945/17185"},"canonical_url":"https://search.dev.ndltd.org/etd/nps/oai:calhoun.nps.edu:10945/17185","repository":{"repo_id":"nps","name":"Naval Postgraduate School","base_url":"https://calhoun.nps.edu/server/oai/request"},"display":{"title":"Projectile thrust-drag optimization with external burning","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.","abstract_html":"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.","abstract_has_math":false,"creators":["Smithey, William John Henry"],"institution":"Monterey, California. Naval Postgraduate School","degree_name":null,"degree_level":null,"degree_discipline":null,"degree_department":"Aeronautics","school":null,"contributors":[],"advisors":["Fuhs, Allen E."],"committee_chairs":[],"committee_members":[],"year":1974,"date_issued":"1974-06","date_published":"1974-06","updated_at":"2026-07-27T20:26:05Z","subjects":[],"languages":["en_US"],"rights":["This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. 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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."]},{"key":"dc:title","label":"Title","values":["Projectile thrust-drag optimization with external burning"]}]}],"canonical_facts":{"dc:contributor.advisor":["Fuhs, Allen E."],"dc:contributor.department":["Aeronautics"],"dc:creator":["Smithey, William John Henry"],"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. 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