Journal of Space Science and Technology

Journal of Space Science and Technology

Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor

Document Type : Original Research Paper

Author
Department of Mechanical Engineering, Faculty of Engineering, Kharazmi University, Tehran, Iran.
Abstract
Trapped vortex combustor (TVC) is a compact combustor which represents the high efficiency in flame stabilization. In this study, turbulent reacting flow through trapped vortex combustor is numerically simulated. In order to model turbulence, the K-ω-SST and scale adaptive simulation (SAS) models, and to model combustion, the species transport and probability density function (PDF) approaches are used. To verify the numerical model, numerical results are compared with the available experimental data. There is a good agreement between the mean and RMS values of temperature and emission indices (CO, unbernt hydrocarbon (UHC) and NOx) obtained from numerical results and experimental data. Moreover, simulation is performed for different values of equivalence ratios and mainstream inlet temperatures and results show that with a constant value of equivalence ratio, by increasing the mainstream inlet temperature, combustion efficiency increases, while CO and UHC emission indices decrease.
Keywords

Article Title Persian

شبیه‌سازی عددی جریان واکنشی مغشوش در محفظة احتراق با گردابة به دام افتاده

Author Persian

مصطفی اسماعیلی
دانشکده مکانیک، دانشکده فنی، دانشگاه خوارزمی، تهران، ایران
Abstract Persian

محفظة احتراق با گردابة به دام افتاده محفظه‌ای فشرده است که کارایی بالایی در پایداری شعله دارد. در این مطالعه، جریان واکنشی مغشوش در محفظة احتراق با گردابة به دام افتاده به صورت عددی شبیه‌سازی شده است. مدل‌های توربولانسی شبیه‌سازی مقیاس انطباقی و K-ω-SST، و رویکردهای احتراقی انتقال اجزاء و تابع چگالی احتمال برای مدل‌سازی توربولانس و احتراق مورد استفاده قرار گرفته‌اند. به منظور اعتبارسنجی مدل عددی، نتایج عددی با نتایج آزمایشگاهی موجود مقایسه شده است. انطباق مناسبی بین مقادیر متوسط و نوسانی دما، مقادیر صدور آلاینده‌ها (مونوکسید کربن، هیدروکربن نسوخته و اکسیدهای نیتروژن) و همچنین راندمان احتراق به‌دست آمده از حل عددی و نتایج آزمایشگاهی وجود دارد. ضمناً، شبیه‌سازی برای مقادیر مختلف نسبت هم ارزی و دمای ورودی جریان اصلی انجام شد و نتایج نشان می‌دهد که در یک مقدار ثابت نسبت هم ارزی، با افزایش دمای جریان اصلی، راندمان احتراق افزایش و شاخص‌های آلایندگی مونوکسیدکربن و هیدروکربن نسوخته کاهش می‌یابند.

Keywords Persian

محفظة احتراق با گردابة به‌دام افتاده
جریان مغشوش
شاخص‌های آلایندگی
راندمان احتراق
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  • Receive Date 15 March 2017
  • Revise Date 06 June 2017
  • Accept Date 02 August 2017
  • First Publish Date 02 August 2017