{"id":393287,"date":"2024-11-08T10:05:36","date_gmt":"2024-11-08T10:05:36","guid":{"rendered":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/total-pressure-data-of-the-simulation-is-not-correct\/"},"modified":"2024-11-08T10:05:36","modified_gmt":"2024-11-08T10:05:36","slug":"total-pressure-data-of-the-simulation-is-not-correct","status":"publish","type":"topic","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/total-pressure-data-of-the-simulation-is-not-correct\/","title":{"rendered":"Total pressure data of the simulation is not correct."},"content":{"rendered":"<p>&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;I have simulated a Supersonic Jet Flow &#8211; Convergent-Divergent nozzle&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;First, the geometry was used without settling chamber but after analyzing the pressure plot a settling chamber was introduced to match exactly as experiment but still the total pressure plot is wrong.&nbsp;&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;1). Boundary conditions used are as follows:&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Settling Chamber Inlet: Pressure Inlet, Total Pressure= 253312.5 Pa &amp; Initial Gauge Pressure = 233312.5 Pa, Total Temp = 300K&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Far-Field Boundary: Pressure Far-Field, Gauge Pressure = 0, Mach = 0.01&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Outlet: Pressure Outlet, Gauge Pressure = 0, Backflow Pressure = Total Pressure&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Operating Pressure = 101325 Pa&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;2). Another simulation has been done and boundary conditions used are as follows:&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Settling Chamber Inlet: Pressure Inlet, Total Pressure= 253312.5 Pa &amp; Initial Gauge Pressure = 0 Pa, Total Temp = 300K&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Far-Field Boundary: Pressure Far-Field, Gauge Pressure = 0, Mach = 0.01&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Outlet: Pressure Outlet, Gauge Pressure = 0, Backflow Pressure = Total Pressure&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Operating Pressure = 101325 Pa&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;3). Another simulation has been done using these Boundary conditions:&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Settling Chamber Inlet: Pressure Inlet, Total Pressure= 253312.5 Pa &amp; Initial Gauge Pressure = 250312.5 Pa, Total Temp = 300K&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Far-Field Boundary: Pressure Far-Field, Gauge Pressure = 0, Mach = 0.01&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Outlet: Pressure Outlet, Gauge Pressure = 0, Backflow Pressure = Total Pressure&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Operating Pressure = 101325 Pa&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Note: Density-Based Steady Solver, SST-kw Model with Low Reynolds Correction, Implicit Formulation, Roe-FDS Flux type and LSCB &amp; Second order Upwind discretization method was adopted.&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Mesh Element: Firstly, 300000 mesh elements were taken but after not getting satisfactory results, number of mesh element was increased 2 to 3 times. In the last simulation, mesh element was about 17Lakhs (1.7M). Fine mesh element (10^-6 m) distributed in near wall region.&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Pseudo Time Method = off : Hybrid Initialization Method adopted&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Solution Steering = On, Used FMG&nbsp;Initialization, Courant Number= 1 to 5&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&nbsp;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Please help me and suggest what is wrong here in my simulation and boundary condition.&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;Please also suggest the correct boundary condition Parameters for NPR = 2.5, 4 &lt;\/span&gt;&lt;span style=&#8221;font-size: 12pt;&#8221;&gt;&amp; 6&lt;\/span&gt;&lt;\/p&gt;&lt;p&gt;<img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/innovationspace.ansys.com\/forum\/wp-content\/uploads\/sites\/2\/2024\/11\/08-11-2024-1731059492-Screenshot (74).png\" alt=\"Mesh and Geometry Model\" width=\"637\" height=\"390\" \/><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/innovationspace.ansys.com\/forum\/wp-content\/uploads\/sites\/2\/2024\/11\/08-11-2024-1731059639-Screenshot (72).png\" alt=\"Mach Number\" width=\"665\" height=\"338\" \/>&lt;\/p&gt;&lt;p&gt;<img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/innovationspace.ansys.com\/forum\/wp-content\/uploads\/sites\/2\/2024\/11\/08-11-2024-1731059698-Screenshot (73).png\" alt=\"Total Pressure\" width=\"651\" height=\"325\" \/><img decoding=\"async\" src=\"https:\/\/innovationspace.ansys.com\/forum\/wp-content\/uploads\/sites\/2\/2024\/11\/08-11-2024-1731059755-Screenshot (71).png\" alt=\"Published Data\" \/>&lt;\/p&gt;<\/p>\n","protected":false},"template":"","class_list":["post-393287","topic","type-topic","status-publish","hentry","topic-tag-c-d-nozzle-2","topic-tag-SupersonicNozzleFlow-1","topic-tag-total-pressure"],"aioseo_notices":[],"aioseo_head":"\n\t\t<!-- All in One SEO 4.9.10 - aioseo.com -->\n\t<meta name=\"description\" content=\"I have simulated a Supersonic Jet Flow - Convergent-Divergent nozzleFirst, the geometry was used without settling chamber but after analyzing the pressure plot a settling chamber was introduced to match exactly as experiment but still the total pressure plot is wrong. 1). 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