


{"id":463072,"date":"2026-08-30T08:26:12","date_gmt":"2026-08-30T08:26:12","guid":{"rendered":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/persistent-high-temperature-pdf-enthalpy-exceedance-traced-to-hot-burnt-pilot\/"},"modified":"2026-08-30T08:26:12","modified_gmt":"2026-08-30T08:26:12","slug":"persistent-high-temperature-pdf-enthalpy-exceedance-traced-to-hot-burnt-pilot","status":"publish","type":"topic","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/persistent-high-temperature-pdf-enthalpy-exceedance-traced-to-hot-burnt-pilot\/","title":{"rendered":"Persistent high-temperature \/ PDF enthalpy exceedance traced to hot burnt pilot"},"content":{"rendered":"<p class=\"PDq2pG_selectionAnchorContainer\" data-start=\"1009\" data-end=\"1294\">I am using Fluent 2022 R2 (v222, build 10212) for a transient LES\/WALE simulation with Partially Premixed Combustion, FGM, C-equation, Non-Adiabatic Energy Treatment and Finite-Rate turbulence-chemistry interaction. Radiation is off. The mesh contains 10.69 million polyhedral cells.<\/p>\n<p data-start=\"1299\" data-end=\"1433\">The physical configuration contains a hot burnt pilot adjacent to the cold premixed burner stream. The pilot must remain in the model.<\/p>\n<p data-start=\"1438\" data-end=\"1465\"><strong data-start=\"1438\" data-end=\"1465\">Current pilot boundary:<\/strong><\/p>\n<ul data-start=\"1468\" data-end=\"1641\">\n<li data-start=\"1468\" data-end=\"1485\" data-section-id=\"1r1emp8\">mass-flow-inlet<\/li>\n<li data-start=\"1488\" data-end=\"1514\" data-section-id=\"kgmt4v\">mass flow = 1.43e-4 kg\/s<\/li>\n<li data-start=\"1517\" data-end=\"1545\" data-section-id=\"1vnuuc2\">Total Temperature = 2000 K<\/li>\n<li data-start=\"1548\" data-end=\"1577\" data-section-id=\"1o5omvt\">Mean Mixture Fraction Z = 1<\/li>\n<li data-start=\"1580\" data-end=\"1616\" data-section-id=\"1jy2071\">normalized Progress Variable C = 1<\/li>\n<li data-start=\"1619\" data-end=\"1639\" data-section-id=\"mrgt1e\">both variances = 0<\/li>\n<\/ul>\n<p data-start=\"1644\" data-end=\"1741\">Z=1 represents the premixed CH4\/air reactant stream at equivalence ratio 0.8; Z=0 is ambient air.<\/p>\n<h3 data-start=\"1746\" data-end=\"1776\" data-section-id=\"pfcr08\">Original numerical symptom<\/h3>\n<p data-start=\"1781\" data-end=\"1943\">We initially investigated persistent <code data-start=\"1818\" data-end=\"1857\">\"Maximum PDF table enthalpy exceeded\"<\/code> warnings and a very large high-temperature population. At a trusted saved checkpoint:<\/p>\n<ul data-start=\"1948\" data-end=\"2173\">\n<li data-start=\"1948\" data-end=\"1979\" data-section-id=\"1ky1p7n\">T &gt; 2200 K: <strong data-start=\"1962\" data-end=\"1979\">607,239 cells<\/strong><\/li>\n<li data-start=\"1982\" data-end=\"2013\" data-section-id=\"1l0m3kx\">T &gt; 2400 K: <strong data-start=\"1996\" data-end=\"2013\">454,109 cells<\/strong><\/li>\n<li data-start=\"2016\" data-end=\"2047\" data-section-id=\"rkxhmq\">T &gt; 2600 K: <strong data-start=\"2030\" data-end=\"2047\">282,747 cells<\/strong><\/li>\n<li data-start=\"2050\" data-end=\"2082\" data-section-id=\"1fa26dw\">T &gt; 2800 K: <strong data-start=\"2064\" data-end=\"2082\">~103,329 cells<\/strong><\/li>\n<li data-start=\"2085\" data-end=\"2171\" data-section-id=\"18c1t0k\">Tmax = <strong data-start=\"2094\" data-end=\"2108\">2849.998 K<\/strong>, exactly the upper temperature limit of the current PDF table.<\/li>\n<\/ul>\n<p data-start=\"2176\" data-end=\"2318\">Of the cells above 2400 K, <strong data-start=\"2203\" data-end=\"2212\">82.3%<\/strong> have cell enthalpy above their local PDF-table maximum enthalpy. Above 2600 K this fraction is <strong data-start=\"2308\" data-end=\"2317\">87.8%<\/strong>.<\/p>\n<h3 data-start=\"2323\" data-end=\"2371\" data-section-id=\"f9tpx6\">Numerical\/model sensitivities already tested<\/h3>\n<p data-start=\"2376\" data-end=\"2543\">We have already performed a substantial set of controlled sensitivity tests, so we would particularly appreciate guidance beyond generic URF\/time-step recommendations:<\/p>\n<ul data-start=\"2548\" data-end=\"4215\">\n<li data-start=\"2548\" data-end=\"2662\" data-section-id=\"fadkz\"><strong data-start=\"2550\" data-end=\"2564\">Time step:<\/strong> reducing dt from 2e-5 to 1e-5 s did not materially change the solution at matched physical times.<\/li>\n<li data-start=\"2665\" data-end=\"2849\" data-section-id=\"1vh4i59\"><strong data-start=\"2667\" data-end=\"2682\">Energy URF:<\/strong> reducing Energy URF from 1.0 to 0.8 produced essentially the same high-temperature population; in a clean sibling comparison it was slightly worse rather than better.<\/li>\n<li data-start=\"2852\" data-end=\"3083\" data-section-id=\"11x8y77\"><strong data-start=\"2854\" data-end=\"2882\">PDF enthalpy resolution:<\/strong> increasing the enthalpy coordinate from <strong data-start=\"2923\" data-end=\"2948\">20 to 80 points (H80)<\/strong> produced only a modest reduction (~5% in T&gt;2400 and ~3% in T&gt;2600 populations at comparable times); the underlying behaviour remained.<\/li>\n<li data-start=\"3086\" data-end=\"3214\" data-section-id=\"q1478b\"><strong data-start=\"3088\" data-end=\"3134\">Adaptive Grid Refinement of the PDF table:<\/strong> AGR = 0.10 changed the high-temperature counts by less than approximately 0.5%.<\/li>\n<li data-start=\"3217\" data-end=\"3463\" data-section-id=\"1cc2w3p\"><strong data-start=\"3219\" data-end=\"3237\">Extrapolation:<\/strong> turning solution extrapolation OFF produced essentially the same result. At the same physical time, T&gt;2200 \/ T&gt;2400 \/ T&gt;2600 counts were 676,287 \/ 485,091 \/ 288,294 versus 671,044 \/ 482,312 \/ 288,988 in the comparison branch.<\/li>\n<li data-start=\"3466\" data-end=\"3600\" data-section-id=\"m5qu0h\"><strong data-start=\"3468\" data-end=\"3491\">Poor-mesh numerics:<\/strong> Poor Mesh Numerics correction was tested and had essentially zero effect on the high-temperature population.<\/li>\n<li data-start=\"3603\" data-end=\"3742\" data-section-id=\"109d9z0\"><strong data-start=\"3605\" data-end=\"3627\">Operating density:<\/strong> changing the specified operating density to a representative value produced essentially identical early behaviour.<\/li>\n<li data-start=\"3745\" data-end=\"3986\" data-section-id=\"93ij9f\"><strong data-start=\"3747\" data-end=\"3786\">Pilot temperature\/flow adjustments:<\/strong> increasing the pilot temperature toward the experimental ~2230 K worsened the PDF-enthalpy warnings; reducing the pilot flow did not eliminate the problem and in one test increased the warning count.<\/li>\n<li data-start=\"3989\" data-end=\"4213\" data-section-id=\"179ahry\"><strong data-start=\"3991\" data-end=\"4011\">Heat-gain range:<\/strong> increasing the heat-gain range moved the PDF temperature ceiling from ~2425 K to ~2850 K, but the solution then populated temperatures up to the new ceiling rather than removing the underlying anomaly.<\/li>\n<\/ul>\n<p data-start=\"4218\" data-end=\"4533\">Global transient mass balance closes to approximately 1% of the net boundary flux. All walls are adiabatic and radiation is off. Therefore we have found no indication that a gross mass imbalance, wall heat input, Energy URF, time step, table resolution, extrapolation, or isolated poor cells are the primary origin.<\/p>\n<h3 data-start=\"4538\" data-end=\"4574\" data-section-id=\"1rdid9s\">Key boundary-enthalpy diagnostic<\/h3>\n<p data-start=\"4579\" data-end=\"4630\">We then measured the pilot boundary state directly.<\/p>\n<p data-start=\"4635\" data-end=\"4660\">On all pilot inlet faces:<\/p>\n<ul data-start=\"4665\" data-end=\"4841\">\n<li data-start=\"4665\" data-end=\"4683\" data-section-id=\"2cmf7z\">F_T = 2000.000 K<\/li>\n<li data-start=\"4686\" data-end=\"4695\" data-section-id=\"1vz39zb\">F_Z = 1<\/li>\n<li data-start=\"4698\" data-end=\"4808\" data-section-id=\"1fdfhiw\">F_PREMIXC = 0.1221857, corresponding to the burnt maximum of the transported un-normalized progress variable<\/li>\n<li data-start=\"4811\" data-end=\"4839\" data-section-id=\"vw3vwu\"><strong data-start=\"4813\" data-end=\"4839\">F_H = +2.015300e6 J\/kg<\/strong><\/li>\n<\/ul>\n<p data-start=\"4844\" data-end=\"4905\">Fluent&#8217;s own native heat-transfer report independently gives:<\/p>\n<p data-start=\"4910\" data-end=\"4966\"><code data-start=\"4910\" data-end=\"4966\">pilot heat-transfer \/ pilot mass-flow = +2.0153e6 J\/kg<\/code><\/p>\n<p data-start=\"4971\" data-end=\"5023\">so this value is not a UDF post-processing artefact.<\/p>\n<p data-start=\"5028\" data-end=\"5168\">However, cells at essentially the same burnt thermochemical state (Z&asymp;1, normalized C&asymp;1, T&asymp;2000&ndash;2050 K, enthalpy inside the PDF bounds) have:<\/p>\n<p data-start=\"5173\" data-end=\"5194\"><strong data-start=\"5173\" data-end=\"5194\">H &asymp; -2.064e5 J\/kg<\/strong><\/p>\n<p data-start=\"5199\" data-end=\"5277\">and <code data-start=\"5203\" data-end=\"5232\">Pdf_Adiabatic_Enthalpy(Z=1)<\/code> also gives approximately <strong data-start=\"5258\" data-end=\"5276\">-2.0644e5 J\/kg<\/strong>.<\/p>\n<p data-start=\"5282\" data-end=\"5333\">Therefore the pilot boundary carries approximately:<\/p>\n<p data-start=\"5338\" data-end=\"5410\"><strong data-start=\"5338\" data-end=\"5410\">+2.219 MJ\/kg more total enthalpy than the corresponding burnt state.<\/strong><\/p>\n<p data-start=\"5415\" data-end=\"5665\">The anomalous enthalpy is already present on the pilot boundary and in the first downstream cell layers, whereas the main heat-release-rate peak occurs farther downstream. Thus the excess enthalpy is not first generated inside the main reaction zone.<\/p>\n<p data-start=\"5670\" data-end=\"6014\">Furthermore, the pilot boundary value <strong data-start=\"5708\" data-end=\"5728\">+2.015300e6 J\/kg<\/strong> agrees almost exactly with an independently measured PDF upper enthalpy value on the <strong data-start=\"5814\" data-end=\"5836\">unburnt (C=0) side<\/strong>, +2.0152998e6 J\/kg. We regard this only as an observation; we have not determined whether it represents clipping\/limiting, a particular T&rarr;H inversion path, or another mechanism.<\/p>\n<p data-start=\"6019\" data-end=\"6260\">The main cold velocity inlet provides a useful sanity check: T=300 K, Z=1, C=0 gives F_H&asymp;-2.0644e5 J\/kg. We recognize that this does not isolate boundary type because the main inlet is a velocity inlet whereas the pilot is a mass-flow inlet.<\/p>\n<h3 data-start=\"6265\" data-end=\"6292\" data-section-id=\"15gviso\">Mesh\/modeling questions<\/h3>\n<p data-start=\"6297\" data-end=\"6689\">The flame-region mesh size is approximately <strong data-start=\"6341\" data-end=\"6352\">0.30 mm<\/strong>. Our estimated laminar flame thickness is approximately <strong data-start=\"6409\" data-end=\"6421\">0.534 mm<\/strong>. Poor-mesh-cell treatment had essentially no effect, but we would like your assessment of whether the spatial resolution itself is inadequate for this Partially Premixed FGM\/C-equation LES formulation and could materially contribute to the observed temperature field.<\/p>\n<p data-start=\"6694\" data-end=\"7044\">More importantly, our PDF table uses <strong data-start=\"6731\" data-end=\"6839\">adiabatic premixed flamelets with the Non-Adiabatic Energy Treatment \/ heat-loss-gain enthalpy extension<\/strong>. Because a ~2000 K fully burnt pilot stream enters immediately adjacent to a ~300 K premixed reactant stream, is this application within the intended validity of that standard non-adiabatic FGM treatment?<\/p>\n<p data-start=\"7049\" data-end=\"7337\">Could the large local enthalpy difference between the hot burnt pilot and cold main stream require <strong data-start=\"7148\" data-end=\"7269\">true non-adiabatic flamelet generation at multiple reference temperatures\/enthalpies (or burner-stabilized flamelets)<\/strong> rather than an adiabatic flamelet manifold with enthalpy extension?<\/p>\n<h3 data-start=\"7342\" data-end=\"7364\" data-section-id=\"ig7vxc\">Requested guidance<\/h3>\n<p data-start=\"7369\" data-end=\"7428\">We would like a specific recommendation for Fluent 2022 R2:<\/p>\n<ol data-start=\"7433\" data-end=\"8351\">\n<li data-start=\"7433\" data-end=\"7534\" data-section-id=\"wy5zyi\">How should a physically required ~2000 K fully burnt pilot be specified in Partially Premixed FGM?<\/li>\n<li data-start=\"7537\" data-end=\"7725\" data-section-id=\"ubmly5\">For a mass-flow inlet with T0=2000 K, Z=1 and normalized C=1, why does Fluent assign approximately +2.0153 MJ\/kg total enthalpy instead of the ~-0.206 MJ\/kg adiabatic burnt-state value?<\/li>\n<li data-start=\"7728\" data-end=\"7851\" data-section-id=\"18xzuwy\">Is this expected behaviour, a known 2022 R2 limitation\/defect, or an incorrect boundary\/model specification on our side?<\/li>\n<li data-start=\"7854\" data-end=\"7917\" data-section-id=\"4axvzu\">Is a different inlet treatment required for the burnt pilot?<\/li>\n<li data-start=\"7920\" data-end=\"7985\" data-section-id=\"ndhfp6\">Is our ~0.30 mm flame-region mesh insufficient for this model?<\/li>\n<li data-start=\"7988\" data-end=\"8192\" data-section-id=\"xzfolp\">For a hot burnt pilot immediately adjacent to a cold premixed burner stream, should we generate genuinely non-adiabatic flamelets instead of using adiabatic flamelets with the heat-loss\/gain extension?<\/li>\n<li data-start=\"8195\" data-end=\"8349\" data-section-id=\"jfqh6p\">What is the recommended correction that preserves the physical pilot and avoids the observed PDF-table enthalpy exceedance\/high-temperature population?<\/li>\n<\/ol>\n<p data-start=\"8354\" data-end=\"8487\">We can provide the full case\/data checkpoint, PDF table, native Fluent flux reports, UDF diagnostic and detailed sensitivity results.<\/p>\n<p data-start=\"8354\" data-end=\"8487\"><img decoding=\"async\" src=\"https:\/\/innovationspace.ansys.com\/forum\/wp-content\/uploads\/sites\/2\/2026\/08\/image-129.png\" alt=\"\"><\/p>\n","protected":false},"template":"","class_list":["post-463072","topic","type-topic","status-publish","hentry","topic-tag-cfd-combustion","topic-tag-fgm","topic-tag-methane-air"],"aioseo_notices":[],"aioseo_head":"\n\t\t<!-- All in One SEO 4.9.10 - aioseo.com -->\n\t<meta name=\"description\" content=\"I am using Fluent 2022 R2 (v222, build 10212) for a transient LES\/WALE simulation with Partially Premixed Combustion, FGM, C-equation, Non-Adiabatic Energy Treatment and Finite-Rate turbulence-chemistry interaction. 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Radiation is off. The mesh contains 10.69 million polyhedral cells. The physical configuration contains a hot burnt pilot adjacent to the cold premixed burner stream. 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The physical configuration contains a hot burnt pilot adjacent to the cold premixed burner stream. The pilot must"},"aioseo_meta_data":[],"aioseo_breadcrumb":"<div class=\"aioseo-breadcrumbs\"><span class=\"aioseo-breadcrumb\">\n\t\t\t<a href=\"https:\/\/innovationspace.ansys.com\/forum\" title=\"Home\">Home<\/a>\n\t\t<\/span><span class=\"aioseo-breadcrumb-separator\">&raquo;<\/span><span class=\"aioseo-breadcrumb\">\n\t\t\t<a href=\"https:\/\/innovationspace.ansys.com\/forum\/topics\/\" title=\"Topics\">Topics<\/a>\n\t\t<\/span><span class=\"aioseo-breadcrumb-separator\">&raquo;<\/span><span class=\"aioseo-breadcrumb\">\n\t\t\t<a href=\"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic-tag\/cfd-combustion\/\" title=\"cfd-combustion\">cfd-combustion<\/a>\n\t\t<\/span><span class=\"aioseo-breadcrumb-separator\">&raquo;<\/span><span class=\"aioseo-breadcrumb\">\n\t\t\tPersistent high-temperature \/ PDF enthalpy exceedance traced to hot burnt pilot\n\t\t<\/span><\/div>","aioseo_breadcrumb_json":[{"label":"Home","link":"https:\/\/innovationspace.ansys.com\/forum"},{"label":"Topics","link":"https:\/\/innovationspace.ansys.com\/forum\/topics\/"},{"label":"cfd-combustion","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic-tag\/cfd-combustion\/"},{"label":"Persistent high-temperature \/ PDF enthalpy exceedance traced to hot burnt pilot","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/persistent-high-temperature-pdf-enthalpy-exceedance-traced-to-hot-burnt-pilot\/"}],"acf":[],"custom_fields":[{"0":{"_bbp_forum_id":["27792"],"_bbp_topic_id":["463072"],"_bbp_subscription":["553792"],"_bbp_author_ip":[null],"_bbp_last_reply_id":["0"],"_bbp_last_active_id":["463072"],"_bbp_last_active_time":["2026-08-30 08:26:12"],"_bbp_reply_count":["0"],"_bbp_reply_count_hidden":["0"],"_bbp_engagement":["1"],"_bbp_likes_count":["0"],"_btv_view_count":["9"],"application":["FLUENT"],"emailnotification":[null],"_bbp_topic_status":["unanswered"]},"test":"can-sumeyyemetu-edu-tr"}],"_links":{"self":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/topics\/463072","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/topics"}],"about":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/types\/topic"}],"version-history":[{"count":0,"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/topics\/463072\/revisions"}],"wp:attachment":[{"href":"https:\/\/innovationspace.ansys.com\/forum\/wp-json\/wp\/v2\/media?parent=463072"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}