Aerodynamic Stability Technology for Maneuverable Missiles. Volume I. Configuration Aerodynamic Characteristics
This study developed empirical methods to predict aerodynamic characteristics of body-tail, body-wing-tail and body-strake-tail missile configurations. Methods cover the Mach number range from 0.6 to 3.0. Methods cover the individual body and tail characteristics at angles of attack from 0 to 180 de...
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| creator | Aiello, Gennaro F Bateman, Michael C |
| description | This study developed empirical methods to predict aerodynamic characteristics of body-tail, body-wing-tail and body-strake-tail missile configurations. Methods cover the Mach number range from 0.6 to 3.0. Methods cover the individual body and tail characteristics at angles of attack from 0 to 180 degrees. For winged bodies the methods encompass angles of attack up to about 30 degrees. All mutual interference effects are accounted for, allowing accurate prediction of force and moment coefficients. (Author)
See also Volume 2, AD-A068 971. |
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See also Volume 2, AD-A068 971.</description><language>eng</language><subject>AERODYNAMIC CHARACTERISTICS ; AERODYNAMIC CONFIGURATIONS ; AERODYNAMIC STABILITY ; Body strake tail configuration ; Body tail configuration ; Body wing tail configuration ; Fluid Mechanics ; FUSELAGES ; Guided Missiles ; MATHEMATICAL PREDICTION ; PE62201F ; Pitch plane ; PITCH(MOTION) ; STRAKES ; TAILS(AIRCRAFT) ; THRUST VECTOR CONTROL SYSTEMS ; WINGS</subject><creationdate>1979</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA070250$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Aiello, Gennaro F</creatorcontrib><creatorcontrib>Bateman, Michael C</creatorcontrib><creatorcontrib>MARTIN MARIETTA AEROSPACE ORLANDO FL</creatorcontrib><title>Aerodynamic Stability Technology for Maneuverable Missiles. Volume I. Configuration Aerodynamic Characteristics</title><description>This study developed empirical methods to predict aerodynamic characteristics of body-tail, body-wing-tail and body-strake-tail missile configurations. Methods cover the Mach number range from 0.6 to 3.0. Methods cover the individual body and tail characteristics at angles of attack from 0 to 180 degrees. For winged bodies the methods encompass angles of attack up to about 30 degrees. All mutual interference effects are accounted for, allowing accurate prediction of force and moment coefficients. (Author)
See also Volume 2, AD-A068 971.</description><subject>AERODYNAMIC CHARACTERISTICS</subject><subject>AERODYNAMIC CONFIGURATIONS</subject><subject>AERODYNAMIC STABILITY</subject><subject>Body strake tail configuration</subject><subject>Body tail configuration</subject><subject>Body wing tail configuration</subject><subject>Fluid Mechanics</subject><subject>FUSELAGES</subject><subject>Guided Missiles</subject><subject>MATHEMATICAL PREDICTION</subject><subject>PE62201F</subject><subject>Pitch plane</subject><subject>PITCH(MOTION)</subject><subject>STRAKES</subject><subject>TAILS(AIRCRAFT)</subject><subject>THRUST VECTOR CONTROL SYSTEMS</subject><subject>WINGS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1979</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFjLEKwjAQQLM4iPoHDvcDlqKIc2gVHTpZXMs1vbQHaQ6SVOjf28HBzekN7_HWSjQF6WaPIxt4JmzZcZqhJjN4cdLPYCVAhZ6mNwVsHUHFMbKjmMFL3DQSPDIoxFvup4CJxcPvsxgwoEkUOCY2catWFl2k3Zcbtb9d6-J-6BbbLImn1OhS55f8eM5Pf_QHjQZATw</recordid><startdate>197903</startdate><enddate>197903</enddate><creator>Aiello, Gennaro F</creator><creator>Bateman, Michael C</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>197903</creationdate><title>Aerodynamic Stability Technology for Maneuverable Missiles. Volume I. Configuration Aerodynamic Characteristics</title><author>Aiello, Gennaro F ; Bateman, Michael C</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA0702503</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1979</creationdate><topic>AERODYNAMIC CHARACTERISTICS</topic><topic>AERODYNAMIC CONFIGURATIONS</topic><topic>AERODYNAMIC STABILITY</topic><topic>Body strake tail configuration</topic><topic>Body tail configuration</topic><topic>Body wing tail configuration</topic><topic>Fluid Mechanics</topic><topic>FUSELAGES</topic><topic>Guided Missiles</topic><topic>MATHEMATICAL PREDICTION</topic><topic>PE62201F</topic><topic>Pitch plane</topic><topic>PITCH(MOTION)</topic><topic>STRAKES</topic><topic>TAILS(AIRCRAFT)</topic><topic>THRUST VECTOR CONTROL SYSTEMS</topic><topic>WINGS</topic><toplevel>online_resources</toplevel><creatorcontrib>Aiello, Gennaro F</creatorcontrib><creatorcontrib>Bateman, Michael C</creatorcontrib><creatorcontrib>MARTIN MARIETTA AEROSPACE ORLANDO FL</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Aiello, Gennaro F</au><au>Bateman, Michael C</au><aucorp>MARTIN MARIETTA AEROSPACE ORLANDO FL</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Aerodynamic Stability Technology for Maneuverable Missiles. Volume I. Configuration Aerodynamic Characteristics</btitle><date>1979-03</date><risdate>1979</risdate><abstract>This study developed empirical methods to predict aerodynamic characteristics of body-tail, body-wing-tail and body-strake-tail missile configurations. Methods cover the Mach number range from 0.6 to 3.0. Methods cover the individual body and tail characteristics at angles of attack from 0 to 180 degrees. For winged bodies the methods encompass angles of attack up to about 30 degrees. All mutual interference effects are accounted for, allowing accurate prediction of force and moment coefficients. (Author)
See also Volume 2, AD-A068 971.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AERODYNAMIC CHARACTERISTICS AERODYNAMIC CONFIGURATIONS AERODYNAMIC STABILITY Body strake tail configuration Body tail configuration Body wing tail configuration Fluid Mechanics FUSELAGES Guided Missiles MATHEMATICAL PREDICTION PE62201F Pitch plane PITCH(MOTION) STRAKES TAILS(AIRCRAFT) THRUST VECTOR CONTROL SYSTEMS WINGS |
| title | Aerodynamic Stability Technology for Maneuverable Missiles. Volume I. Configuration Aerodynamic Characteristics |
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