Invariant Methods of Determining the Lift Coefficient of Various Aerodynamic Profiles According to the Flow Spectrum
Invariant methods are used in wind tunnels and aerodynamic installations with visualization of part of the flow pattern encompassing the necessary section with the characteristic line of flow; in wind tunnels in which visualization is not possible for various reasons; in preliminary studies of a lar...
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| creator | Suprun,V M |
| description | Invariant methods are used in wind tunnels and aerodynamic installations with visualization of part of the flow pattern encompassing the necessary section with the characteristic line of flow; in wind tunnels in which visualization is not possible for various reasons; in preliminary studies of a large number of promising types of mechanization (UPS (boundary layer control), pumping or blowing of jet), for which the development of special complex equipment is required for the feeding and exhausting of air through a weighing system and in physical studies of new circulation two-dimensional flows around aerodynamic contours caused by various reasons.
Edited trans. of Samoletostroenie i Tekhnika Vozdushnogo Flota (USSR) n25 p8-14 1971, by Louise E. Heenan. |
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Edited trans. of Samoletostroenie i Tekhnika Vozdushnogo Flota (USSR) n25 p8-14 1971, by Louise E. Heenan.</description><subject>COEFFICIENTS</subject><subject>FLUID FLOW</subject><subject>Fluid Mechanics</subject><subject>INVARIANCE</subject><subject>LEADING EDGES</subject><subject>LIFT</subject><subject>TRANSLATIONS</subject><subject>USSR</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1973</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFjMEKwjAQRHvxIOofeNgfEIo99Fxai4KCoHgtIdm0C01Wkq3i3xuKd08DM-_NMpOTf6lAygtcUAY2EdhCg4LBkSffgwwIZ7ICNaO1pAkTm5hH0niKUGFg8_HKkYZrYEsjplJrDmbWeX5oR37D7YlawuTW2cKqMeLml6ts2x7u9XFnhHQXhTxKVzV5We7zvCj-zF-JRUE8</recordid><startdate>19731130</startdate><enddate>19731130</enddate><creator>Suprun,V M</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19731130</creationdate><title>Invariant Methods of Determining the Lift Coefficient of Various Aerodynamic Profiles According to the Flow Spectrum</title><author>Suprun,V M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD07720033</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1973</creationdate><topic>COEFFICIENTS</topic><topic>FLUID FLOW</topic><topic>Fluid Mechanics</topic><topic>INVARIANCE</topic><topic>LEADING EDGES</topic><topic>LIFT</topic><topic>TRANSLATIONS</topic><topic>USSR</topic><toplevel>online_resources</toplevel><creatorcontrib>Suprun,V M</creatorcontrib><creatorcontrib>FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Suprun,V M</au><aucorp>FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Invariant Methods of Determining the Lift Coefficient of Various Aerodynamic Profiles According to the Flow Spectrum</btitle><date>1973-11-30</date><risdate>1973</risdate><abstract>Invariant methods are used in wind tunnels and aerodynamic installations with visualization of part of the flow pattern encompassing the necessary section with the characteristic line of flow; in wind tunnels in which visualization is not possible for various reasons; in preliminary studies of a large number of promising types of mechanization (UPS (boundary layer control), pumping or blowing of jet), for which the development of special complex equipment is required for the feeding and exhausting of air through a weighing system and in physical studies of new circulation two-dimensional flows around aerodynamic contours caused by various reasons.
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| language | eng |
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| source | DTIC Technical Reports |
| subjects | COEFFICIENTS FLUID FLOW Fluid Mechanics INVARIANCE LEADING EDGES LIFT TRANSLATIONS USSR |
| title | Invariant Methods of Determining the Lift Coefficient of Various Aerodynamic Profiles According to the Flow Spectrum |
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