Transonic Flow Fields Around Various Bodies of Revolution Including Preliminary Studies on Viscous Effects with and without Plume
The report outlines the solution to the lifting slender body in transonic flow. Remarks are also made concerning the transonic flow past cone- cylindrical configurations. Preliminary calculations concerning viscous effects, and particularly plume induced separation, are included.
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creator | Wu, Jain-Ming Aoyama, Kinya Moulden, Trevor H |
description | The report outlines the solution to the lifting slender body in transonic flow. Remarks are also made concerning the transonic flow past cone- cylindrical configurations. Preliminary calculations concerning viscous effects, and particularly plume induced separation, are included. |
format | Report |
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Remarks are also made concerning the transonic flow past cone- cylindrical configurations. Preliminary calculations concerning viscous effects, and particularly plume induced separation, are included.</description><language>eng</language><subject>ANGLE OF ATTACK ; BOUNDARY LAYER ; Combustion and Ignition ; CONICAL BODIES ; CYLINDRICAL BODIES ; EQUATIONS OF MOTION ; EXHAUST FLAMES ; EXPERIMENTAL DATA ; FLOW SEPARATION ; Fluid Mechanics ; Guided Missiles ; inviscid flow ; MATHEMATICAL ANALYSIS ; missile plumes ; SLENDER BODIES ; TRANSONIC CHARACTERISTICS ; VISCOSITY</subject><creationdate>1971</creationdate><rights>Approved for public release; distribution is unlimited.</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/AD0729335$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Wu, Jain-Ming</creatorcontrib><creatorcontrib>Aoyama, Kinya</creatorcontrib><creatorcontrib>Moulden, Trevor H</creatorcontrib><creatorcontrib>TENNESSEE UNIV SPACE INST TULLAHOMA</creatorcontrib><title>Transonic Flow Fields Around Various Bodies of Revolution Including Preliminary Studies on Viscous Effects with and without Plume</title><description>The report outlines the solution to the lifting slender body in transonic flow. Remarks are also made concerning the transonic flow past cone- cylindrical configurations. Preliminary calculations concerning viscous effects, and particularly plume induced separation, are included.</description><subject>ANGLE OF ATTACK</subject><subject>BOUNDARY LAYER</subject><subject>Combustion and Ignition</subject><subject>CONICAL BODIES</subject><subject>CYLINDRICAL BODIES</subject><subject>EQUATIONS OF MOTION</subject><subject>EXHAUST FLAMES</subject><subject>EXPERIMENTAL DATA</subject><subject>FLOW SEPARATION</subject><subject>Fluid Mechanics</subject><subject>Guided Missiles</subject><subject>inviscid flow</subject><subject>MATHEMATICAL ANALYSIS</subject><subject>missile plumes</subject><subject>SLENDER BODIES</subject><subject>TRANSONIC CHARACTERISTICS</subject><subject>VISCOSITY</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1971</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFjL0KwkAQhNNYiPoGFvsCghhELKMmaBdU0objbk8XLrtwPwZL31yD9lYz8M034-x19YqDMGmonPRQEToToPCS2ECjPEkKsBNDGEAsnPEhLkUShhNrlwzxDWqPjjpi5Z9wiem7ZWgo6MEurUUdA_QU76A-t0ORFKF2qcNpNrLKBZz9cpLNq_K6Py5MJN2GSIyxLQ7LzWqb5-v8D34DicRGiQ</recordid><startdate>19710527</startdate><enddate>19710527</enddate><creator>Wu, Jain-Ming</creator><creator>Aoyama, Kinya</creator><creator>Moulden, Trevor H</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19710527</creationdate><title>Transonic Flow Fields Around Various Bodies of Revolution Including Preliminary Studies on Viscous Effects with and without Plume</title><author>Wu, Jain-Ming ; Aoyama, Kinya ; Moulden, Trevor H</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD07293353</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1971</creationdate><topic>ANGLE OF ATTACK</topic><topic>BOUNDARY LAYER</topic><topic>Combustion and Ignition</topic><topic>CONICAL BODIES</topic><topic>CYLINDRICAL BODIES</topic><topic>EQUATIONS OF MOTION</topic><topic>EXHAUST FLAMES</topic><topic>EXPERIMENTAL DATA</topic><topic>FLOW SEPARATION</topic><topic>Fluid Mechanics</topic><topic>Guided Missiles</topic><topic>inviscid flow</topic><topic>MATHEMATICAL ANALYSIS</topic><topic>missile plumes</topic><topic>SLENDER BODIES</topic><topic>TRANSONIC CHARACTERISTICS</topic><topic>VISCOSITY</topic><toplevel>online_resources</toplevel><creatorcontrib>Wu, Jain-Ming</creatorcontrib><creatorcontrib>Aoyama, Kinya</creatorcontrib><creatorcontrib>Moulden, Trevor H</creatorcontrib><creatorcontrib>TENNESSEE UNIV SPACE INST TULLAHOMA</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Wu, Jain-Ming</au><au>Aoyama, Kinya</au><au>Moulden, Trevor H</au><aucorp>TENNESSEE UNIV SPACE INST TULLAHOMA</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Transonic Flow Fields Around Various Bodies of Revolution Including Preliminary Studies on Viscous Effects with and without Plume</btitle><date>1971-05-27</date><risdate>1971</risdate><abstract>The report outlines the solution to the lifting slender body in transonic flow. Remarks are also made concerning the transonic flow past cone- cylindrical configurations. Preliminary calculations concerning viscous effects, and particularly plume induced separation, are included.</abstract><oa>free_for_read</oa></addata></record> |
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source | DTIC Technical Reports |
subjects | ANGLE OF ATTACK BOUNDARY LAYER Combustion and Ignition CONICAL BODIES CYLINDRICAL BODIES EQUATIONS OF MOTION EXHAUST FLAMES EXPERIMENTAL DATA FLOW SEPARATION Fluid Mechanics Guided Missiles inviscid flow MATHEMATICAL ANALYSIS missile plumes SLENDER BODIES TRANSONIC CHARACTERISTICS VISCOSITY |
title | Transonic Flow Fields Around Various Bodies of Revolution Including Preliminary Studies on Viscous Effects with and without Plume |
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