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			<title>Development</title>
			<link>typhon-cfd-solver/development//</link>
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				<title>Development</title>
				<url>https://websites.isae-supaero.fr/local/cache-vignettes/L144xH30/rubon201-032cb.png?1775089118</url>
				<link>typhon-cfd-solver/development//</link>
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		<title>Planned developments</title>
		<link>https://websites.isae-supaero.fr/typhon-cfd-solver/development/planned-developments</link>
		<guid isPermaLink="true">https://websites.isae-supaero.fr/typhon-cfd-solver/development/planned-developments</guid>
		<dc:date>2009-06-03T12:00:00Z</dc:date>
		<dc:format>text/html</dc:format>
		<dc:language>en</dc:language>
		<dc:creator>GRESSIER J&#233;r&#233;mie</dc:creator>



		<description>
&lt;p&gt;Here is a non exhaustive list of short term planned developments. Core project FeatureAssigned developerStatus Periodic boundary conditions J. Gressier done Normalized residuals J. Gressier done Probe history based of volumic data J. Gressier done End of computation with total number of iterations Memory efficient splitting method Vectorisation of symbolic functions J. Gressier CFD tools FeatureAssigned developerStatus Face based tags in cgns reading J. Gressier open (...)&lt;/p&gt;


-
&lt;a href="https://websites.isae-supaero.fr/typhon-cfd-solver/development/" rel="directory"&gt;Development&lt;/a&gt;


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 <content:encoded>&lt;div class='rss_texte'&gt;&lt;p&gt;Here is a non exhaustive list of &lt;i&gt;short term&lt;/i&gt; planned developments.&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;Core project&lt;/h3&gt;&lt;table class=&#034;spip&#034;&gt;
&lt;thead&gt;&lt;tr class='row_first'&gt;&lt;th id='idd477_c0'&gt;Feature&lt;/th&gt;&lt;th id='idd477_c1'&gt;Assigned developer&lt;/th&gt;&lt;th id='idd477_c2'&gt;Status&lt;/th&gt;&lt;/tr&gt;&lt;/thead&gt;
&lt;tbody&gt;
&lt;tr class='row_odd odd'&gt;
&lt;td headers='idd477_c0'&gt;Periodic boundary conditions&lt;/td&gt;
&lt;td headers='idd477_c1'&gt;J. Gressier&lt;/td&gt;
&lt;td headers='idd477_c2'&gt;done&lt;/td&gt;&lt;/tr&gt;
&lt;tr class='row_even even'&gt;
&lt;td headers='idd477_c0'&gt;Normalized residuals&lt;/td&gt;
&lt;td headers='idd477_c1'&gt;J. Gressier&lt;/td&gt;
&lt;td headers='idd477_c2'&gt;done&lt;/td&gt;&lt;/tr&gt;
&lt;tr class='row_odd odd'&gt;
&lt;td headers='idd477_c0'&gt;Probe history based of volumic data&lt;/td&gt;
&lt;td headers='idd477_c1'&gt;J. Gressier&lt;/td&gt;
&lt;td headers='idd477_c2'&gt;done&lt;/td&gt;&lt;/tr&gt;
&lt;tr class='row_even even'&gt;
&lt;td headers='idd477_c0'&gt;End of computation with total number of iterations&lt;/td&gt;
&lt;td headers='idd477_c1'&gt;&lt;/td&gt;
&lt;td headers='idd477_c2'&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr class='row_odd odd'&gt;
&lt;td headers='idd477_c0'&gt;Memory efficient splitting method&lt;/td&gt;
&lt;td headers='idd477_c1'&gt;&lt;/td&gt;
&lt;td headers='idd477_c2'&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr class='row_even even'&gt;
&lt;td headers='idd477_c0'&gt;Vectorisation of symbolic functions&lt;/td&gt;
&lt;td headers='idd477_c1'&gt;J. Gressier&lt;/td&gt;
&lt;td headers='idd477_c2'&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/tbody&gt;
&lt;/table&gt;&lt;h3 class=&#034;spip&#034;&gt;CFD tools&lt;/h3&gt;&lt;table class=&#034;spip&#034;&gt;
&lt;thead&gt;&lt;tr class='row_first'&gt;&lt;th id='ideaba_c0'&gt;Feature&lt;/th&gt;&lt;th id='ideaba_c1'&gt;Assigned developer&lt;/th&gt;&lt;th id='ideaba_c2'&gt;Status&lt;/th&gt;&lt;/tr&gt;&lt;/thead&gt;
&lt;tbody&gt;
&lt;tr class='row_odd odd'&gt;
&lt;td headers='ideaba_c0'&gt;Face based tags in cgns reading&lt;/td&gt;
&lt;td headers='ideaba_c1'&gt;J. Gressier&lt;/td&gt;
&lt;td headers='ideaba_c2'&gt;open&lt;/td&gt;&lt;/tr&gt;
&lt;tr class='row_even even'&gt;
&lt;td headers='ideaba_c0'&gt;internal mesh format&lt;/td&gt;
&lt;td headers='ideaba_c1'&gt;J. Gressier&lt;/td&gt;
&lt;td headers='ideaba_c2'&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/tbody&gt;
&lt;/table&gt;&lt;h3 class=&#034;spip&#034;&gt;Navier-Stokes solver&lt;/h3&gt;&lt;table class=&#034;spip&#034;&gt;
&lt;thead&gt;&lt;tr class='row_first'&gt;&lt;th id='idf16e_c0'&gt;Feature&lt;/th&gt;&lt;th id='idf16e_c1'&gt;Assigned developer&lt;/th&gt;&lt;th id='idf16e_c2'&gt;Status&lt;/th&gt;&lt;/tr&gt;&lt;/thead&gt;
&lt;tbody&gt;
&lt;tr class='row_odd odd'&gt;
&lt;td headers='idf16e_c0'&gt;Source terms (gravity)&lt;/td&gt;
&lt;td headers='idf16e_c1'&gt;&lt;/td&gt;
&lt;td class='numeric ' headers='idf16e_c2'&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr class='row_even even'&gt;
&lt;td headers='idf16e_c0'&gt;SVM viscous flux&lt;/td&gt;
&lt;td headers='idf16e_c1'&gt;O. Chikhaoui&lt;/td&gt;
&lt;td class='numeric ' headers='idf16e_c2'&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr class='row_odd odd'&gt;
&lt;td headers='idf16e_c0'&gt;SVM TVD/TVB limitation&lt;/td&gt;
&lt;td headers='idf16e_c1'&gt;O. Chikhaoui&lt;/td&gt;
&lt;td class='numeric ' headers='idf16e_c2'&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr class='row_even even'&gt;
&lt;td headers='idf16e_c0'&gt;Axisymmetric solver&lt;/td&gt;
&lt;td headers='idf16e_c1'&gt;&lt;/td&gt;
&lt;td class='numeric ' headers='idf16e_c2'&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/tbody&gt;
&lt;/table&gt;&lt;h3 class=&#034;spip&#034;&gt;Heat transfer solver&lt;/h3&gt;&lt;table class=&#034;spip&#034;&gt;
&lt;thead&gt;&lt;tr class='row_first'&gt;&lt;th id='ida55b_c0'&gt;Feature&lt;/th&gt;&lt;th id='ida55b_c1'&gt;Assigned developer&lt;/th&gt;&lt;th id='ida55b_c2'&gt;Status&lt;/th&gt;&lt;/tr&gt;&lt;/thead&gt;
&lt;tbody&gt;
&lt;tr class='row_odd odd'&gt;
&lt;th class='numeric ' headers='ida55b_c0' id='ida55b_l0'&gt;&lt;/th&gt;
&lt;td class='numeric ' headers='ida55b_c1 ida55b_l0'&gt;&lt;/td&gt;
&lt;td class='numeric ' headers='ida55b_c2 ida55b_l0'&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/tbody&gt;
&lt;/table&gt;&lt;/div&gt;
		
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				<item xml:lang="en">
		<title>Developers</title>
		<link>https://websites.isae-supaero.fr/typhon-cfd-solver/development/developers</link>
		<guid isPermaLink="true">https://websites.isae-supaero.fr/typhon-cfd-solver/development/developers</guid>
		<dc:date>2009-05-24T13:30:00Z</dc:date>
		<dc:format>text/html</dc:format>
		<dc:language>en</dc:language>
		<dc:creator>GRESSIER J&#233;r&#233;mie</dc:creator>



		<description>
&lt;p&gt;Project Administrators &lt;br class='autobr' /&gt; J. Gressier Main Developers &lt;br class='autobr' /&gt; J. Gressier (ISAE)
&lt;br class='autobr' /&gt; G. Grondin (ISAE) Contributors &lt;br class='autobr' /&gt; O. Chikhaoui (SVM)
&lt;br class='autobr' /&gt; A. Gardi (MRF, ALE)
&lt;br class='autobr' /&gt; G. Lavalle (axisymmetric source terms)
&lt;br class='autobr' /&gt; E. Radenac (as PhD student)
&lt;br class='autobr' /&gt; Praveen
&lt;br class='autobr' /&gt; H. Gagnon
&lt;br class='autobr' /&gt; A. Blay, J. Rodriguez, N. Morbieu, M. Betoule (as Supaero students)&lt;/p&gt;


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&lt;a href="https://websites.isae-supaero.fr/typhon-cfd-solver/development/" rel="directory"&gt;Development&lt;/a&gt;


		</description>


 <content:encoded>&lt;div class='rss_texte'&gt;&lt;h3 class=&#034;spip&#034;&gt;Project Administrators&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; &lt;a href=&#034;http://pagespro.isae.fr/jeremie-gressier&#034; class='spip_out' rel='external'&gt;J. Gressier&lt;/a&gt;&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;Main Developers&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; &lt;a href=&#034;http://pagespro.isae.fr/jeremie-gressier&#034; class='spip_out' rel='external'&gt;J. Gressier&lt;/a&gt; (ISAE)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; G. Grondin (ISAE)&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;Contributors&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; O. Chikhaoui (SVM)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; A. Gardi (MRF, ALE)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; G. Lavalle (axisymmetric source terms)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; E. Radenac (as PhD student)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Praveen
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; H. Gagnon
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; A. Blay, J. Rodriguez, N. Morbieu, M. Betoule (as Supaero students)&lt;/p&gt;&lt;/div&gt;
		
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				<item xml:lang="en">
		<title>Change log</title>
		<link>https://websites.isae-supaero.fr/typhon-cfd-solver/development/change-log</link>
		<guid isPermaLink="true">https://websites.isae-supaero.fr/typhon-cfd-solver/development/change-log</guid>
		<dc:date>2009-05-10T19:00:00Z</dc:date>
		<dc:format>text/html</dc:format>
		<dc:language>en</dc:language>
		<dc:creator>GRESSIER J&#233;r&#233;mie</dc:creator>



		<description>
&lt;p&gt;release 0.5.0 (r632)	2009/03/10 NS Spectral Volume Method (3rd &amp; 4th order, VTK output) (r602-603,618-619,624-625) NS Kinetic flux function (EFM/KFVS) (r631) and Rusanov flux (r612) NS Post-limitation (Barth, Monotonic) (r610,623) Mesh SVM-like mesh splitting (r618-619,624-625) KDIF Unsteady non uniform boundary conditions (symbolic functions) (r601) KDIF Implicitation of Flux and Thermal conditions (r612) KDIF Inverse boundary condition solver (r606,607,609,613-615,617,620) Core (...)&lt;/p&gt;


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&lt;a href="https://websites.isae-supaero.fr/typhon-cfd-solver/development/" rel="directory"&gt;Development&lt;/a&gt;


		</description>


 <content:encoded>&lt;div class='rss_texte'&gt;&lt;h3 class=&#034;spip&#034;&gt;release 0.5.0 (r632)	2009/03/10&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Spectral Volume Method (3rd &amp; 4th order, VTK output) (r602-603,618-619,624-625)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Kinetic flux function (EFM/KFVS) (r631) and Rusanov flux (r612)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Post-limitation (Barth, Monotonic) (r610,623)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Mesh SVM-like mesh splitting (r618-619,624-625)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF Unsteady non uniform boundary conditions (symbolic functions) (r601)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF Implicitation of Flux and Thermal conditions (r612)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF Inverse boundary condition solver (r606,607,609,613-615,617,620)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core GMRES solver (NS or KDIF) (r627)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core Improvement of memory management (r621)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Input Improve CGNS reading (r601)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core translations of comments (r627)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core generalized element connectivity (r602)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Ouput remove NODE based Tecplot output (r602)&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.4.0 (r600)	2008/03/21&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Spectral Volume Method (2nd order) (r597-599)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Runge Kutta integration (RK2, RK3-SSP) (r592,594)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Miscellaneous initialization modes (r591,594)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Mesh SVM2QUAD splitting for all methods (r589-590)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MPI portage (r576,578)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Input Improve CGNS reading (unused marks, volume marks) (r590-591)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Input Intel fortran 9.1 portage (CGNS reading) (r593)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Ouput Screen outputs enhancement (r582,586)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Ouput Miscellaneous translations (r570-575,577)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core tree/list structure of unstructured grids (r562)&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.3.2 (r559)	2007/02/06&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Basic MUSCL method (MUSCL-UNS)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Initialization with symbolic functions
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Initialization with optional static/total pressure or temperature, Mach/velocity
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Moving wall boundary condition (WALL_VELOCITY)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Viscous flux implicitation
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Output Binary VTK (VTK-BIN)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core Automatic system configuration
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core Automatic non regression test cases&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.3.1 (r479)	2006/08/26&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Kim's 3rd order limiter extended to MUSCL method
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Output display CPU time
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Output enhanced outputs and options (periodic, etc)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core external stop of computation (file stop_typhon)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core CPU optimization (20% for explicit second order NS computation)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core symbolic computation library
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MESH can use long file names
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MPI Bug correction in automatic splitting&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.3.0 (r406)	2006/03/05&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MPI automatic mesh splitting (Metis)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MPI NS first order computation (up to 20 procs at least)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MPI NS second order computation (slightly different results at interfaces)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MPI Unsteady synchronization&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.2.2	2006/01/16&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Opt optimization of CPU cost for gradient optimization (nearly 50%)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Fast MUSCL method (for high quality meshes)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Kim's 3rd order limiter (only for Fast MUSCL method)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS test of internal energy positivity (output of bad cell index if not positive)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; Core ensure local time stepping bounded to cycle time step&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.3 RC 1	2005/11/06&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MPI automatic mesh splitting (Metis)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MPI NS first order computation (up to 20 procs)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MPI Unsteady synchronization&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.2.1	13/10/2005&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MESH scaling function
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features constant dynamic viscosity
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features linear dynamic viscosity
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS initialization with a file
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF initialization with a file
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS improved subsonic outlet condition (enforce pi&gt;= p)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features Implicit jacobian matrices for HLL fluxes (diagonal equivalent)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS improved MUSCL method
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features non-uniform thermal boundary conditions
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS improved heat flux boundary condition at wall
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; core Navier-Stokes/Heat transfer coupling
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS CFL computation for unsteady problems&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.2.0	04/09/2005&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MESH scaling function
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features constant dynamic viscosity
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; core Implicitation program structure reorganised (include ghost cells)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF features BiCG, BiCG-Jacobi, CGS iterative inversion methods (DLU structure)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF improved adiabatic boundary condition
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features BiCG-Stab iterative inversion method (block-DLU structure)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS changed symmetry boundary condition (ghost cell is now really symmetric: improved hypersonic flows)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features (validation) Viscous stress tensor (laminar flows), Sutherland law
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features increasing CFL number with convergence (bounded by CFL_MAX parameter)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS MUSCL interpolation for second order accuracy
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features non-uniform thermal boundary conditions
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS improved heat flux boundary condition at wall
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; core Navier-Stokes/Heat transfer coupling&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.1.7	08/07/2005&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; core introduces User Defined Functions (UDF) through user-made fortran functions
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF features radiating boundary condition
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF features radiative coupling with view factors (simplified)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF features anisotropic material (only UDF)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF features boundary parameters temporal interpolation (via UDF)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features HLLC upwind scheme (ability for viscous flows)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS features Viscous stress tensor (laminar flows)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; OUTPUT can write boundary condition face centers
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; OUTPUT can write unsteady results on boundaring family&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.1.6	10/12/2004&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS MUSCL interpolation for 2nd order computations
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; GUI Plot residuals for only one zone
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; OUTPUT Residuals in monres.nnn file&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.1.5	05/08/2004&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS Inviscid solver released, HLLE first order upwind scheme
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS boundary conditions: subsonic and supersonic inlet and oulet
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; NS boundary conditions: symmetry
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; OUTPUT VTK format for scalars and vectors (NS only)&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.1.4	01/07/2004&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; known bug computation of 3D meshes with QUAD face cells
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MESH CGNS files: TRI/QUAD 2D meshes, TETRA/PRISM 3D meshes
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF boundary conditions: convection h(T-Tref)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF Implicit time integration (direct LU or Iterative Jacobi)
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; OUTPUT VTK format for scalars and vectors (NS only)&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.1.3	08/04/2004&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; known bug computation of gradients
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MESH CGNS files: 2D meshes of TRI cells
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MZONE KDIF/KDIF coupling
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MZONE Computation of conformal connections of faces between zones&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.1.2	15/10/2003&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; INPUT Manage stationnary computations by residual criteria
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; core Computation of gradients by least mean square method
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; core CPU optimization
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF extended flux interpolation
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF Fourier based timestep computation&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.1.1	01/08/2003&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; OUTPUT TECPLOT files, vertex based solution (QUAD) and connectivity&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;release 0.1.0	01/07/2003&lt;/h3&gt;
&lt;p&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; MESH CGNS files: unstructured 2D mesh of QUAD cells
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF Heat transfer solver released
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF constant conduction coefficient
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF explicit temporal integration with global time step
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF simplified flux interpolation
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; KDIF boundary conditions: isothermal and adiabatic
&lt;br /&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L8xH11/puce-32883.gif?1775035618' width='8' height='11' class='puce' alt=&#034;-&#034; /&gt; OUTPUT TECPLOT files, cell centered solution&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;june 2002: started development&lt;/h3&gt;&lt;/div&gt;
		
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