Stall Speed
Aerodynamic stall is one of the most safety‐critical performance limits of an aircraft and must be verified by direct measurement early in a flight test campaign. This chapter provides a summary of the theory of aerodynamic stall, including a brief discussion of boundary layer separation, two‐dimens...
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creator | Liu, Tianshu Gregory, James W |
description | Aerodynamic stall is one of the most safety‐critical performance limits of an aircraft and must be verified by direct measurement early in a flight test campaign. This chapter provides a summary of the theory of aerodynamic stall, including a brief discussion of boundary layer separation, two‐dimensional stall, and three‐dimensional wing stall. A brief overview of analytical approaches to estimating stall speed is provided before turning to flight test techniques. Piloting, data acquisition, and data reduction techniques for stall are discussed, including an example of stall speed measurement for a Cirrus SR20. |
doi_str_mv | 10.1002/9781118949818.ch12 |
format | Book Chapter |
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This chapter provides a summary of the theory of aerodynamic stall, including a brief discussion of boundary layer separation, two‐dimensional stall, and three‐dimensional wing stall. A brief overview of analytical approaches to estimating stall speed is provided before turning to flight test techniques. Piloting, data acquisition, and data reduction techniques for stall are discussed, including an example of stall speed measurement for a Cirrus SR20.</description><identifier>ISBN: 111894982X</identifier><identifier>ISBN: 9781118949825</identifier><identifier>EISBN: 111894979X</identifier><identifier>EISBN: 9781118949795</identifier><identifier>EISBN: 9781118949818</identifier><identifier>EISBN: 1118949811</identifier><identifier>DOI: 10.1002/9781118949818.ch12</identifier><identifier>OCLC: 1251441246</identifier><identifier>LCCallNum: TL671.7 .G74 2021</identifier><language>eng</language><publisher>United Kingdom: John Wiley & Sons, Incorporated</publisher><subject>aerodynamic stall ; boundary layer ; maximum lift coefficient ; separation ; stall speed ; tufts</subject><ispartof>Introduction to Flight Testing, 2021, p.205-223</ispartof><rights>2021 John Wiley & Sons Ltd.</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttps://ebookcentral.proquest.com/covers/6607709-l.jpg</thumbnail><link.rule.ids>779,780,784,793,27925</link.rule.ids></links><search><contributor>Gregory, James</contributor><contributor>Liu, Tianshu</contributor><creatorcontrib>Liu, Tianshu</creatorcontrib><creatorcontrib>Gregory, James W</creatorcontrib><title>Stall Speed</title><title>Introduction to Flight Testing</title><description>Aerodynamic stall is one of the most safety‐critical performance limits of an aircraft and must be verified by direct measurement early in a flight test campaign. This chapter provides a summary of the theory of aerodynamic stall, including a brief discussion of boundary layer separation, two‐dimensional stall, and three‐dimensional wing stall. A brief overview of analytical approaches to estimating stall speed is provided before turning to flight test techniques. Piloting, data acquisition, and data reduction techniques for stall are discussed, including an example of stall speed measurement for a Cirrus SR20.</description><subject>aerodynamic stall</subject><subject>boundary layer</subject><subject>maximum lift coefficient</subject><subject>separation</subject><subject>stall speed</subject><subject>tufts</subject><isbn>111894982X</isbn><isbn>9781118949825</isbn><isbn>111894979X</isbn><isbn>9781118949795</isbn><isbn>9781118949818</isbn><isbn>1118949811</isbn><fulltext>true</fulltext><rsrctype>book_chapter</rsrctype><creationdate>2021</creationdate><recordtype>book_chapter</recordtype><recordid>eNpVj01Lw0AQhldEUWP_gCf_QOrM7ia7c5TiFxQ8tIfelv2YUDXYmI2I_97UFMHLzLwDzwuPEFcIcwSQN2QsIlrSZNHO4xblkbg4fAxtjv-ClZvTMcgKtUap6zMxy_kVxg5dVYbUuShWg2_b61XHnC7FSePbzLPDLsT6_m69eCyXzw9Pi9tl2VmSpSclUSKxCRhBsSUYjxqSUoghUFTWNsiYgpcNm1jXNiViwAApJi9VIdRU-_XS8rfjsNu9ZYfg9m7un5vbu_2OkdIT1fW7j0_OwwRGfh9638at7wbus6trMAbIoa6cVKh-AA5DULo</recordid><startdate>2021</startdate><enddate>2021</enddate><creator>Liu, Tianshu</creator><creator>Gregory, James W</creator><general>John Wiley & Sons, Incorporated</general><general>John Wiley & Sons, Ltd</general><scope>FFUUA</scope></search><sort><creationdate>2021</creationdate><title>Stall Speed</title><author>Liu, Tianshu ; Gregory, James W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p892-a9321219e7b1c03e890b1c60d3311bb9c388f1e1dba2fe7c668dd9e01b0dcda23</frbrgroupid><rsrctype>book_chapters</rsrctype><prefilter>book_chapters</prefilter><language>eng</language><creationdate>2021</creationdate><topic>aerodynamic stall</topic><topic>boundary layer</topic><topic>maximum lift coefficient</topic><topic>separation</topic><topic>stall speed</topic><topic>tufts</topic><toplevel>online_resources</toplevel><creatorcontrib>Liu, Tianshu</creatorcontrib><creatorcontrib>Gregory, James W</creatorcontrib><collection>ProQuest Ebook Central - Book Chapters - Demo use only</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Liu, Tianshu</au><au>Gregory, James W</au><au>Gregory, James</au><au>Liu, Tianshu</au><format>book</format><genre>bookitem</genre><ristype>CHAP</ristype><atitle>Stall Speed</atitle><btitle>Introduction to Flight Testing</btitle><date>2021</date><risdate>2021</risdate><spage>205</spage><epage>223</epage><pages>205-223</pages><isbn>111894982X</isbn><isbn>9781118949825</isbn><eisbn>111894979X</eisbn><eisbn>9781118949795</eisbn><eisbn>9781118949818</eisbn><eisbn>1118949811</eisbn><abstract>Aerodynamic stall is one of the most safety‐critical performance limits of an aircraft and must be verified by direct measurement early in a flight test campaign. This chapter provides a summary of the theory of aerodynamic stall, including a brief discussion of boundary layer separation, two‐dimensional stall, and three‐dimensional wing stall. A brief overview of analytical approaches to estimating stall speed is provided before turning to flight test techniques. Piloting, data acquisition, and data reduction techniques for stall are discussed, including an example of stall speed measurement for a Cirrus SR20.</abstract><cop>United Kingdom</cop><pub>John Wiley & Sons, Incorporated</pub><doi>10.1002/9781118949818.ch12</doi><oclcid>1251441246</oclcid><tpages>19</tpages></addata></record> |
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source | Ebook Central - Academic Complete; Ebook Central Perpetual and DDA |
subjects | aerodynamic stall boundary layer maximum lift coefficient separation stall speed tufts |
title | Stall Speed |
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