Solar concentrating technologies can produce heat for applications such as solar heating, solar cooling, industrial processes, desalination and electric power generation. For a solar dish collector, various solar receivers and working fluids at different flow rates can be used in different applications. In this work, three different cavity receivers are investigated for application in a solar dish collector using either water or Behran oil. A numerical model is used in the analysis, which is validated with experimental results from a hemispherical cavity receiver using oil as working fluid. The model is applied to compare hemispherical, cylindrical and cubical receivers under the same operating conditions using either water or oil, at a volumetric flow rate of 100 ml/s and solar irradiance of 800 W/m(2), in order to determine the most suitable cavity for a specific solar dish. The system is investigated for inlet temperatures ranging from 40 degrees C to 90 degrees C with water as working fluid, and from 40 degrees C to 300 degrees C with Behran oil as working fluid. Emphasis is placed on the calculation of useful heat production, as well as pressure drop which influences pumping power. The exergetic efficiency criterion and the overall efficiency criterion are used in order to evaluate the useful heat production and the pumping power simultaneously. The high exergetic efficiency of the hemispherical cavity with thermal oil at high temperatures makes this case a promising choice for high-temperature solar dish collector applications. Moreover, water is found to be the best candidate for low-temperature applications since it leads to the higher thermal efficiency with lower pumping power demand. (C) 2018 Elsevier Ltd. All rights reserved.
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Sharif Univ Technol, Sharif Energy Water & Environm Inst SEWEI, Tehran 1459777611, Iran
Univ Tehran, Fac Governance, Dept Energy Governance, POB 14398 14151, Tehran, IranSharif Univ Technol, Sharif Energy Water & Environm Inst SEWEI, Tehran 1459777611, Iran
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Univ Malaya, Fac Engn, Dept Mech Engn, Kuala Lumpur 50603, MalaysiaUniv Malaya, Fac Engn, Dept Mech Engn, Kuala Lumpur 50603, Malaysia
Aslfattahi, Navid
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Loni, Reyhaneh
Bellos, Evangelos
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Natl Tech Univ Athens, Sch Mech Engn, Thermal Dept, Athens, GreeceUniv Malaya, Fac Engn, Dept Mech Engn, Kuala Lumpur 50603, Malaysia
Bellos, Evangelos
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Najafi, Gholamhassan
Kadirgama, K.
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Univ Malaysia Pahang, Fac Mech & Automot Engn Technol, Pekan, MalaysiaUniv Malaya, Fac Engn, Dept Mech Engn, Kuala Lumpur 50603, Malaysia
Kadirgama, K.
Harun, W. S. W.
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Univ Malaysia Pahang, Fac Mech & Automot Engn Technol, Pekan, MalaysiaUniv Malaya, Fac Engn, Dept Mech Engn, Kuala Lumpur 50603, Malaysia
Harun, W. S. W.
Saidur, R.
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Sunway Univ, Res Ctr Nanomat & Energy Technol RCNMET, Sch Engn & Technol, Petaling Jaya 47500, Selangor Darul, Malaysia
Univ Lancaster, Dept Engn, Lancaster LA1 4YW, EnglandUniv Malaya, Fac Engn, Dept Mech Engn, Kuala Lumpur 50603, Malaysia
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Indian Inst Technol, Dept Mech Engn, Heat Transfer & Thermal Power Lab, Madras 600036, Tamil Nadu, IndiaIndian Inst Technol, Dept Mech Engn, Heat Transfer & Thermal Power Lab, Madras 600036, Tamil Nadu, India
Reddy, K. S.
Kumar, N. Sendhil
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Indian Inst Technol, Dept Mech Engn, Heat Transfer & Thermal Power Lab, Madras 600036, Tamil Nadu, IndiaIndian Inst Technol, Dept Mech Engn, Heat Transfer & Thermal Power Lab, Madras 600036, Tamil Nadu, India
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Department of Aerospace Engineering, Ryerson University, Toronto,ON,M5B 2K3, CanadaDepartment of Aerospace Engineering, Ryerson University, Toronto,ON,M5B 2K3, Canada
Rostami, Mohsen
Pirvaram, Atousa
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Department of Mechanical Engineering, Lassonde School of Engineering, York University, Toronto,ON,M3J 1P3, CanadaDepartment of Aerospace Engineering, Ryerson University, Toronto,ON,M5B 2K3, Canada
Pirvaram, Atousa
Talebzadeh, Nima
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Department of Mechanical Engineering, Lassonde School of Engineering, York University, Toronto,ON,M3J 1P3, CanadaDepartment of Aerospace Engineering, Ryerson University, Toronto,ON,M5B 2K3, Canada
Talebzadeh, Nima
O'Brien, Paul G.
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Department of Mechanical Engineering, Lassonde School of Engineering, York University, Toronto,ON,M3J 1P3, CanadaDepartment of Aerospace Engineering, Ryerson University, Toronto,ON,M5B 2K3, Canada