{"id":364704,"date":"2024-04-29T13:35:39","date_gmt":"2024-04-29T13:35:39","guid":{"rendered":"\/forum\/forums\/reply\/364704\/"},"modified":"2024-04-29T13:35:39","modified_gmt":"2024-04-29T13:35:39","slug":"364704","status":"publish","type":"reply","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/364704\/","title":{"rendered":"Reply To: High-Velocity Air Flow Through Small Nozzle into Large Tank"},"content":{"rendered":"<p>&lt;p&gt;I&#8217;m considering pressures between 20&#8217;000 Pa and 140&#8217;000 Pa. But, since my inlet area is grater than the nozzle one, the flow is subsonic at the inlet. In this condition, the simulations should not be affected by the value of Supersonic\/Initial Gauge Pressure, right?&lt;\/p&gt;<\/p>\n","protected":false},"template":"","class_list":["post-364704","reply","type-reply","status-publish","hentry"],"aioseo_notices":[],"aioseo_head":"\n\t\t<!-- All in One SEO 4.9.10 - aioseo.com -->\n\t<meta name=\"description\" content=\"I&#039;m considering pressures between 20&#039;000 Pa and 140&#039;000 Pa. But, since my inlet area is grater than the nozzle one, the flow is subsonic at the inlet. In this condition, the simulations should not be affected by the value of Supersonic\/Initial Gauge Pressure, right?\" \/>\n\t<meta name=\"robots\" content=\"max-image-preview:large\" \/>\n\t<link rel=\"canonical\" href=\"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/364704\/\" \/>\n\t<meta name=\"generator\" content=\"All in One SEO (AIOSEO) 4.9.10\" \/>\n\t\t<meta property=\"og:locale\" content=\"en_US\" \/>\n\t\t<meta property=\"og:site_name\" content=\"Ansys Learning Forum | Ansys Innovation Space\" \/>\n\t\t<meta property=\"og:type\" content=\"article\" \/>\n\t\t<meta property=\"og:title\" content=\"Reply To: High-Velocity Air Flow Through Small Nozzle into Large Tank | Ansys Learning Forum\" \/>\n\t\t<meta property=\"og:description\" content=\"I&#039;m considering pressures between 20&#039;000 Pa and 140&#039;000 Pa. But, since my inlet area is grater than the nozzle one, the flow is subsonic at the inlet. In this condition, the simulations should not be affected by the value of Supersonic\/Initial Gauge Pressure, right?\" \/>\n\t\t<meta property=\"og:url\" content=\"https:\/\/innovationspace.ansys.com\/forum\/forums\/reply\/364704\/\" \/>\n\t\t<meta property=\"article:published_time\" content=\"2024-04-29T13:35:39+00:00\" \/>\n\t\t<meta property=\"article:modified_time\" content=\"2024-04-29T13:35:39+00:00\" \/>\n\t\t<meta name=\"twitter:card\" content=\"summary_large_image\" \/>\n\t\t<meta name=\"twitter:title\" content=\"Reply To: High-Velocity Air Flow Through Small Nozzle into Large Tank | Ansys Learning Forum\" \/>\n\t\t<meta name=\"twitter:description\" content=\"I&#039;m considering pressures between 20&#039;000 Pa and 140&#039;000 Pa. But, since my inlet area is grater than the nozzle one, the flow is subsonic at the inlet. In this condition, the simulations should not be affected by the value of Supersonic\/Initial Gauge Pressure, right?\" \/>\n\t\t<script type=\"application\/ld+json\" class=\"aioseo-schema\">\n\t\t\t{\"@context\":\"https:\\\/\\\/schema.org\",\"@graph\":[{\"@type\":\"BreadcrumbList\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/364704\\\/#breadcrumblist\",\"itemListElement\":[{\"@type\":\"ListItem\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum#listItem\",\"position\":1,\"name\":\"Home\",\"item\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\",\"nextItem\":{\"@type\":\"ListItem\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/364704\\\/#listItem\",\"name\":\"Reply To: High-Velocity Air Flow Through Small Nozzle into Large Tank\"}},{\"@type\":\"ListItem\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/364704\\\/#listItem\",\"position\":2,\"name\":\"Reply To: High-Velocity Air Flow Through Small Nozzle into Large Tank\",\"previousItem\":{\"@type\":\"ListItem\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum#listItem\",\"name\":\"Home\"}}]},{\"@type\":\"Organization\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/#organization\",\"name\":\"Ansys Learning Forum\",\"description\":\"Ansys Innovation Space\",\"url\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/\"},{\"@type\":\"WebPage\",\"@id\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/364704\\\/#webpage\",\"url\":\"https:\\\/\\\/innovationspace.ansys.com\\\/forum\\\/forums\\\/reply\\\/364704\\\/\",\"name\":\"Reply To: High-Velocity Air Flow Through Small Nozzle into Large Tank | Ansys Learning Forum\",\"description\":\"I'm considering pressures between 20'000 Pa and 140'000 Pa. 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