Loading…
Clarification of "Turn Performance of Aircraft"
A recent note analyzed the minimum turning radius of an airplane in terms of its airspeed and angle of bank. Unfortunately, some misconceptions concerning the underlying physics were introduced. This note is intended to clarify those areas.
Saved in:
| Published in: | SIAM review 1996-06, Vol.38 (2), p.309-312 |
|---|---|
| Main Author: | |
| Format: | Article |
| Language: | English |
| Subjects: | |
| Citations: | Items that this one cites Items that cite this one |
| Online Access: | Get full text |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| cited_by | cdi_FETCH-LOGICAL-c333t-218c7fad4e86a8e9f9c19381ea09b3ea35813c1f8072fab26f4b1a41052968bf3 |
|---|---|
| cites | cdi_FETCH-LOGICAL-c333t-218c7fad4e86a8e9f9c19381ea09b3ea35813c1f8072fab26f4b1a41052968bf3 |
| container_end_page | 312 |
| container_issue | 2 |
| container_start_page | 309 |
| container_title | SIAM review |
| container_volume | 38 |
| creator | Ford, William F. |
| description | A recent note analyzed the minimum turning radius of an airplane in terms of its airspeed and angle of bank. Unfortunately, some misconceptions concerning the underlying physics were introduced. This note is intended to clarify those areas. |
| doi_str_mv | 10.1137/1038045 |
| format | article |
| fullrecord | <record><control><sourceid>jstor_proqu</sourceid><recordid>TN_cdi_proquest_journals_194200000</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><jstor_id>2132884</jstor_id><sourcerecordid>2132884</sourcerecordid><originalsourceid>FETCH-LOGICAL-c333t-218c7fad4e86a8e9f9c19381ea09b3ea35813c1f8072fab26f4b1a41052968bf3</originalsourceid><addsrcrecordid>eNo9kE9LAzEQxYMoWFfxC3goRfC0NpPJ7ibHUvwHBT3U8zIbE9jSNnWyPfjtTWnpaZh5P2bmPSHuQT4DYDMFiUbq6kKMQNqqbJSUl2IkJdYlaF1di5uUVjL3Bu1ITOdr4j70joY-bscxjCfLPW_HX55D5A1tnT8MZz07pjBMbsVVoHXyd6daiO_Xl-X8vVx8vn3MZ4vSIeJQKjCuCfSjvanJeBusA4sGPEnboSesDKCDYGSjAnWqDroD0iArZWvTBSzE5Lh3x_F379PQrmL-K59swers6eCgEE9HyHFMiX1od9xviP9akO0hjPYURiYfT-soOVoHzsb6dMYRsFYKMvZwxFZpiHyWs6KM0fgP5rpkAg</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>194200000</pqid></control><display><type>article</type><title>Clarification of "Turn Performance of Aircraft"</title><source>SIAM Journals Archive</source><source>JSTOR Archival Journals and Primary Sources Collection</source><creator>Ford, William F.</creator><creatorcontrib>Ford, William F.</creatorcontrib><description>A recent note analyzed the minimum turning radius of an airplane in terms of its airspeed and angle of bank. Unfortunately, some misconceptions concerning the underlying physics were introduced. This note is intended to clarify those areas.</description><identifier>ISSN: 0036-1445</identifier><identifier>EISSN: 1095-7200</identifier><identifier>DOI: 10.1137/1038045</identifier><identifier>CODEN: SIREAD</identifier><language>eng</language><publisher>Philadelphia, PA: Society for Industrial and Applied Mathematics</publisher><subject>Aerodynamic lift ; Aerodynamics ; Aircraft ; Aircraft performance ; Aircraft wings ; Airspeed ; Altitude ; Classroom Notes ; Compressible flows; shock and detonation phenomena ; Critical values ; Exact sciences and technology ; Flight paths ; Fluid dynamics ; Fundamental areas of phenomenology (including applications) ; General subsonic flows ; Mathematics ; Physics ; Stall ; Vehicular flight</subject><ispartof>SIAM review, 1996-06, Vol.38 (2), p.309-312</ispartof><rights>Copyright 1996 Society for Industrial and Applied Mathematics</rights><rights>1996 INIST-CNRS</rights><rights>Copyright Society for Industrial and Applied Mathematics Jun 1996</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c333t-218c7fad4e86a8e9f9c19381ea09b3ea35813c1f8072fab26f4b1a41052968bf3</citedby><cites>FETCH-LOGICAL-c333t-218c7fad4e86a8e9f9c19381ea09b3ea35813c1f8072fab26f4b1a41052968bf3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.jstor.org/stable/pdf/2132884$$EPDF$$P50$$Gjstor$$H</linktopdf><linktohtml>$$Uhttps://www.jstor.org/stable/2132884$$EHTML$$P50$$Gjstor$$H</linktohtml><link.rule.ids>314,780,784,3185,27924,27925,58238,58471</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=3136221$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Ford, William F.</creatorcontrib><title>Clarification of "Turn Performance of Aircraft"</title><title>SIAM review</title><description>A recent note analyzed the minimum turning radius of an airplane in terms of its airspeed and angle of bank. Unfortunately, some misconceptions concerning the underlying physics were introduced. This note is intended to clarify those areas.</description><subject>Aerodynamic lift</subject><subject>Aerodynamics</subject><subject>Aircraft</subject><subject>Aircraft performance</subject><subject>Aircraft wings</subject><subject>Airspeed</subject><subject>Altitude</subject><subject>Classroom Notes</subject><subject>Compressible flows; shock and detonation phenomena</subject><subject>Critical values</subject><subject>Exact sciences and technology</subject><subject>Flight paths</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>General subsonic flows</subject><subject>Mathematics</subject><subject>Physics</subject><subject>Stall</subject><subject>Vehicular flight</subject><issn>0036-1445</issn><issn>1095-7200</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1996</creationdate><recordtype>article</recordtype><recordid>eNo9kE9LAzEQxYMoWFfxC3goRfC0NpPJ7ibHUvwHBT3U8zIbE9jSNnWyPfjtTWnpaZh5P2bmPSHuQT4DYDMFiUbq6kKMQNqqbJSUl2IkJdYlaF1di5uUVjL3Bu1ITOdr4j70joY-bscxjCfLPW_HX55D5A1tnT8MZz07pjBMbsVVoHXyd6daiO_Xl-X8vVx8vn3MZ4vSIeJQKjCuCfSjvanJeBusA4sGPEnboSesDKCDYGSjAnWqDroD0iArZWvTBSzE5Lh3x_F379PQrmL-K59swers6eCgEE9HyHFMiX1od9xviP9akO0hjPYURiYfT-soOVoHzsb6dMYRsFYKMvZwxFZpiHyWs6KM0fgP5rpkAg</recordid><startdate>19960601</startdate><enddate>19960601</enddate><creator>Ford, William F.</creator><general>Society for Industrial and Applied Mathematics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>JQ2</scope><scope>U9A</scope></search><sort><creationdate>19960601</creationdate><title>Clarification of "Turn Performance of Aircraft"</title><author>Ford, William F.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c333t-218c7fad4e86a8e9f9c19381ea09b3ea35813c1f8072fab26f4b1a41052968bf3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1996</creationdate><topic>Aerodynamic lift</topic><topic>Aerodynamics</topic><topic>Aircraft</topic><topic>Aircraft performance</topic><topic>Aircraft wings</topic><topic>Airspeed</topic><topic>Altitude</topic><topic>Classroom Notes</topic><topic>Compressible flows; shock and detonation phenomena</topic><topic>Critical values</topic><topic>Exact sciences and technology</topic><topic>Flight paths</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>General subsonic flows</topic><topic>Mathematics</topic><topic>Physics</topic><topic>Stall</topic><topic>Vehicular flight</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ford, William F.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>ProQuest Computer Science Collection</collection><jtitle>SIAM review</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ford, William F.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Clarification of "Turn Performance of Aircraft"</atitle><jtitle>SIAM review</jtitle><date>1996-06-01</date><risdate>1996</risdate><volume>38</volume><issue>2</issue><spage>309</spage><epage>312</epage><pages>309-312</pages><issn>0036-1445</issn><eissn>1095-7200</eissn><coden>SIREAD</coden><abstract>A recent note analyzed the minimum turning radius of an airplane in terms of its airspeed and angle of bank. Unfortunately, some misconceptions concerning the underlying physics were introduced. This note is intended to clarify those areas.</abstract><cop>Philadelphia, PA</cop><pub>Society for Industrial and Applied Mathematics</pub><doi>10.1137/1038045</doi><tpages>4</tpages><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0036-1445 |
| ispartof | SIAM review, 1996-06, Vol.38 (2), p.309-312 |
| issn | 0036-1445 1095-7200 |
| language | eng |
| recordid | cdi_proquest_journals_194200000 |
| source | SIAM Journals Archive; JSTOR Archival Journals and Primary Sources Collection |
| subjects | Aerodynamic lift Aerodynamics Aircraft Aircraft performance Aircraft wings Airspeed Altitude Classroom Notes Compressible flows shock and detonation phenomena Critical values Exact sciences and technology Flight paths Fluid dynamics Fundamental areas of phenomenology (including applications) General subsonic flows Mathematics Physics Stall Vehicular flight |
| title | Clarification of "Turn Performance of Aircraft" |
| url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-03T08%3A46%3A29IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-jstor_proqu&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Clarification%20of%20%22Turn%20Performance%20of%20Aircraft%22&rft.jtitle=SIAM%20review&rft.au=Ford,%20William%20F.&rft.date=1996-06-01&rft.volume=38&rft.issue=2&rft.spage=309&rft.epage=312&rft.pages=309-312&rft.issn=0036-1445&rft.eissn=1095-7200&rft.coden=SIREAD&rft_id=info:doi/10.1137/1038045&rft_dat=%3Cjstor_proqu%3E2132884%3C/jstor_proqu%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c333t-218c7fad4e86a8e9f9c19381ea09b3ea35813c1f8072fab26f4b1a41052968bf3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=194200000&rft_id=info:pmid/&rft_jstor_id=2132884&rfr_iscdi=true |