{"id":221316,"date":"2025-05-29T11:58:46","date_gmt":"2025-05-29T11:58:46","guid":{"rendered":"https:\/\/learnexams.com\/blog\/?p=221316"},"modified":"2025-05-29T11:58:58","modified_gmt":"2025-05-29T11:58:58","slug":"13-47-methane-ch4-at-25c-enters-the-combustor-of-a-simple-open-gas-turbine-power-plant-and-burns-completely-with-400-of-theoretical-air-entering-the-compressor-at-25c-1-atm-5","status":"publish","type":"post","link":"https:\/\/www.learnexams.com\/blog\/2025\/05\/29\/13-47-methane-ch4-at-25c-enters-the-combustor-of-a-simple-open-gas-turbine-power-plant-and-burns-completely-with-400-of-theoretical-air-entering-the-compressor-at-25c-1-atm-5\/","title":{"rendered":"13.47 Methane (CH4), at 25\u00b0C, enters the combustor of a simple open gas turbine power plant and burns completely with 400% of theoretical air entering the compressor at 25\u00b0C, 1 atm."},"content":{"rendered":"\n<p>13.47 Methane (CH4), at 25\u00b0C, enters the combustor of a simple open gas turbine power plant and burns completely with 400% of theoretical air entering the compressor at 25\u00b0C, 1 atm. Products of combustion exit the turbine at 577\u00b0C, 1 atm. The rate of heat transfer from the gas turbine is estimated as 10% of the net power developed. Determine the net power output, in MW, if the fuel mass flow rate is 1200 kg\/h. Kinetic and potential energy effects are negligible.<\/p>\n\n\n\n\n\n\n\n<p><strong><mark style=\"background-color:rgba(0, 0, 0, 0)\" class=\"has-inline-color has-ast-global-color-1-color\">The Correct Answer and Explanation is:<\/mark><\/strong><\/p>\n\n\n\n<p>To solve this problem, we&#8217;ll perform an energy balance around the gas turbine system using the First Law of Thermodynamics. Here&#8217;s a step-by-step explanation followed by the correct numerical solution.<\/p>\n\n\n\n<hr class=\"wp-block-separator has-alpha-channel-opacity\"\/>\n\n\n\n<h3 class=\"wp-block-heading\"><strong>Given Data:<\/strong><\/h3>\n\n\n\n<ul class=\"wp-block-list\">\n<li>Fuel: Methane (CH\u2084)<\/li>\n\n\n\n<li>Fuel flow rate: 1200 kg\/h = 0.3333 kg\/s<\/li>\n\n\n\n<li>Air supply: 400% of theoretical air<\/li>\n\n\n\n<li>Inlet conditions: 25\u00b0C, 1 atm<\/li>\n\n\n\n<li>Exit conditions: 577\u00b0C, 1 atm<\/li>\n\n\n\n<li>Heat loss = 10% of net power output<\/li>\n\n\n\n<li>Kinetic and potential energy changes are negligible<\/li>\n<\/ul>\n\n\n\n<hr class=\"wp-block-separator has-alpha-channel-opacity\"\/>\n\n\n\n<h3 class=\"wp-block-heading\"><strong>Step 1: Combustion Reaction<\/strong><\/h3>\n\n\n\n<p>Complete combustion of methane with stoichiometric air: CH4+2(O2+3.76N2)\u2192CO2+2H2O+7.52N2\\text{CH}_4 + 2(\\text{O}_2 + 3.76\\text{N}_2) \\rightarrow \\text{CO}_2 + 2\\text{H}_2\\text{O} + 7.52\\text{N}_2<\/p>\n\n\n\n<p>For 400% theoretical air, we multiply all air species by 4: CH4+8(O2+3.76N2)\u2192CO2+2H2O+8O2+30.08N2\\text{CH}_4 + 8(\\text{O}_2 + 3.76\\text{N}_2) \\rightarrow \\text{CO}_2 + 2\\text{H}_2\\text{O} + 8\\text{O}_2 + 30.08\\text{N}_2<\/p>\n\n\n\n<p>Total products (per mole CH\u2084):<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>1 CO\u2082<\/li>\n\n\n\n<li>2 H\u2082O<\/li>\n\n\n\n<li>8 O\u2082<\/li>\n\n\n\n<li>30.08 N\u2082<\/li>\n<\/ul>\n\n\n\n<hr class=\"wp-block-separator has-alpha-channel-opacity\"\/>\n\n\n\n<h3 class=\"wp-block-heading\"><strong>Step 2: Enthalpy Change<\/strong><\/h3>\n\n\n\n<p>Use average specific heat capacities CpC_p (ideal gas assumption) and \u0394T = 577\u00b0C \u2212 25\u00b0C = 552 K:<\/p>\n\n\n\n<p>Approximate CpC_p values at average temperature (~300\u2013800 K):<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>CO\u2082: 1.10 kJ\/kg\u00b7K, MW = 44<\/li>\n\n\n\n<li>H\u2082O(g): 2.00 kJ\/kg\u00b7K, MW = 18<\/li>\n\n\n\n<li>O\u2082: 1.00 kJ\/kg\u00b7K, MW = 32<\/li>\n\n\n\n<li>N\u2082: 1.04 kJ\/kg\u00b7K, MW = 28<\/li>\n<\/ul>\n\n\n\n<p>Calculate enthalpy change per kmol CH\u2084: \u0394H=\u2211niCp,i\u0394T\\Delta H = \\sum n_i C_{p,i} \\Delta T \u0394H=(1)(1.10)(552)+(2)(2.00)(552)+(8)(1.00)(552)+(30.08)(1.04)(552)\\Delta H = (1)(1.10)(552) + (2)(2.00)(552) + (8)(1.00)(552) + (30.08)(1.04)(552) \u0394H=607.2+2208+4416+17286.3=24517.5&nbsp;kJ\/kmol&nbsp;CH\u2084\\Delta H = 607.2 + 2208 + 4416 + 17286.3 = 24517.5 \\text{ kJ\/kmol CH\u2084}<\/p>\n\n\n\n<hr class=\"wp-block-separator has-alpha-channel-opacity\"\/>\n\n\n\n<h3 class=\"wp-block-heading\"><strong>Step 3: Convert to per second basis<\/strong><\/h3>\n\n\n\n<p>Molecular weight of CH\u2084 = 16 g\/mol = 16 kg\/kmol<br>So moles\/s of CH\u2084 = 0.333316=0.02083\\frac{0.3333}{16} = 0.02083 kmol\/s<\/p>\n\n\n\n<p>Energy per second (total output before losses): W\u02d9gross=0.02083\u00d724517.5=510.5&nbsp;kW\\dot{W}_{gross} = 0.02083 \\times 24517.5 = 510.5 \\text{ kW}<\/p>\n\n\n\n<hr class=\"wp-block-separator has-alpha-channel-opacity\"\/>\n\n\n\n<h3 class=\"wp-block-heading\"><strong>Step 4: Account for Heat Loss<\/strong><\/h3>\n\n\n\n<p>Only 90% of this is net power output: W\u02d9net=510.51.1=464.1&nbsp;kW=0.464&nbsp;MW\\dot{W}_{net} = \\frac{510.5}{1.1} = 464.1 \\text{ kW} = \\boxed{0.464 \\text{ MW}}<\/p>\n\n\n\n<hr class=\"wp-block-separator has-alpha-channel-opacity\"\/>\n\n\n\n<h3 class=\"wp-block-heading\"><strong>Final Answer:<\/strong><\/h3>\n\n\n\n<p>Net&nbsp;power&nbsp;output=0.464&nbsp;MW\\boxed{\\text{Net power output} = 0.464 \\text{ MW}}<\/p>\n\n\n\n<hr class=\"wp-block-separator has-alpha-channel-opacity\"\/>\n\n\n\n<h3 class=\"wp-block-heading\"><strong>Explanation ):<\/strong><\/h3>\n\n\n\n<p>This problem involves analyzing a gas turbine power plant where methane is combusted with excess air. The energy released from combustion is partially converted to useful mechanical work, with some losses. The First Law of Thermodynamics (energy conservation) is applied here in a control volume around the combustor and turbine.<\/p>\n\n\n\n<p>We first established the combustion equation, accounting for 400% theoretical air, meaning five times the stoichiometric air amount. The combustion produces CO\u2082, H\u2082O, unused O\u2082, and N\u2082. The total enthalpy change of the products, from inlet to exit temperature, determines the energy made available for work. We estimated this enthalpy change using average specific heat capacities over the temperature range from 25\u00b0C to 577\u00b0C.<\/p>\n\n\n\n<p>Using the fuel flow rate, we calculated the number of kilomoles of methane combusted per second. This allowed us to find the total energy released per second (or power) using the enthalpy of the exhaust gases.<\/p>\n\n\n\n<p>However, not all of this power is converted to net mechanical power, as 10% is lost via heat transfer. Therefore, we corrected for this loss to find the net useful power output.<\/p>\n\n\n\n<p>Ultimately, this thermodynamic analysis yielded a net power output of 0.464 MW for a methane fuel flow rate of 1200 kg\/h. This kind of analysis is essential in designing efficient power generation systems and estimating performance from basic operational parameters.<\/p>\n\n\n\n<figure class=\"wp-block-image size-full\"><img decoding=\"async\" src=\"https:\/\/learnexams.com\/blog\/wp-content\/uploads\/2025\/05\/learnexams-banner6-128.jpeg\" alt=\"\" class=\"wp-image-221319\"\/><\/figure>\n","protected":false},"excerpt":{"rendered":"<p>13.47 Methane (CH4), at 25\u00b0C, enters the combustor of a simple open gas turbine power plant and burns completely with 400% of theoretical air entering the compressor at 25\u00b0C, 1 atm. Products of combustion exit the turbine at 577\u00b0C, 1 atm. The rate of heat transfer from the gas turbine is estimated as 10% of [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"site-sidebar-layout":"default","site-content-layout":"","ast-site-content-layout":"default","site-content-style":"default","site-sidebar-style":"default","ast-global-header-display":"","ast-banner-title-visibility":"","ast-main-header-display":"","ast-hfb-above-header-display":"","ast-hfb-below-header-display":"","ast-hfb-mobile-header-display":"","site-post-title":"","ast-breadcrumbs-content":"","ast-featured-img":"","footer-sml-layout":"","ast-disable-related-posts":"","theme-transparent-header-meta":"","adv-header-id-meta":"","stick-header-meta":"","header-above-stick-meta":"","header-main-stick-meta":"","header-below-stick-meta":"","astra-migrate-meta-layouts":"default","ast-page-background-enabled":"default","ast-page-background-meta":{"desktop":{"background-color":"","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"tablet":{"background-color":"","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"mobile":{"background-color":"","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""}},"ast-content-background-meta":{"desktop":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"tablet":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""},"mobile":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center center","background-size":"auto","background-attachment":"scroll","background-type":"","background-media":"","overlay-type":"","overlay-color":"","overlay-opacity":"","overlay-gradient":""}},"footnotes":""},"categories":[25],"tags":[],"class_list":["post-221316","post","type-post","status-publish","format-standard","hentry","category-exams-certification"],"_links":{"self":[{"href":"https:\/\/www.learnexams.com\/blog\/wp-json\/wp\/v2\/posts\/221316","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.learnexams.com\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.learnexams.com\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.learnexams.com\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/www.learnexams.com\/blog\/wp-json\/wp\/v2\/comments?post=221316"}],"version-history":[{"count":0,"href":"https:\/\/www.learnexams.com\/blog\/wp-json\/wp\/v2\/posts\/221316\/revisions"}],"wp:attachment":[{"href":"https:\/\/www.learnexams.com\/blog\/wp-json\/wp\/v2\/media?parent=221316"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.learnexams.com\/blog\/wp-json\/wp\/v2\/categories?post=221316"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.learnexams.com\/blog\/wp-json\/wp\/v2\/tags?post=221316"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}