Projectile thrust-drag optimization with external burning

Approved for public release; distribution unlimited. === 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...

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Main Author:	Smithey, William John Henry
Other Authors:	Fuhs, Allen E.
Language:	en_US
Published:	Monterey, California. Naval Postgraduate School 2012
Online Access:	http://hdl.handle.net/10945/17185

id	ndltd-nps.edu-oai-calhoun.nps.edu-10945-17185
record_format	oai_dc
spelling	ndltd-nps.edu-oai-calhoun.nps.edu-10945-171852015-05-06T03:58:34Z Projectile thrust-drag optimization with external burning Smithey, William John Henry Fuhs, Allen E. Naval Postgraduate School Aeronautics Approved for public release; distribution unlimited. 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. 2012-11-14T00:00:23Z 2012-11-14T00:00:23Z 1974-06 Thesis http://hdl.handle.net/10945/17185 en_US 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. Monterey, California. Naval Postgraduate School
collection	NDLTD
language	en_US
sources	NDLTD
description	Approved for public release; distribution unlimited. === 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.
author2	Fuhs, Allen E.
author_facet	Fuhs, Allen E. Smithey, William John Henry
author	Smithey, William John Henry
spellingShingle	Smithey, William John Henry Projectile thrust-drag optimization with external burning
author_sort	Smithey, William John Henry
title	Projectile thrust-drag optimization with external burning
title_short	Projectile thrust-drag optimization with external burning
title_full	Projectile thrust-drag optimization with external burning
title_fullStr	Projectile thrust-drag optimization with external burning
title_full_unstemmed	Projectile thrust-drag optimization with external burning
title_sort	projectile thrust-drag optimization with external burning
publisher	Monterey, California. Naval Postgraduate School
publishDate	2012
url	http://hdl.handle.net/10945/17185
work_keys_str_mv	AT smitheywilliamjohnhenry projectilethrustdragoptimizationwithexternalburning
_version_	1716803228497084416

Projectile thrust-drag optimization with external burning

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