Please note that all the papers submitted to JAFM, after revision and prior to acceptance, will be checked with iThenticate, a powerful plagiarism detection software, in order to guarantee the quality of papers being published in JAFM. The papers with 20% or more similarities with any other published journal papers will be rejected.
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2017 Vol. 10, No. 5

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Journal of Applied Fluid Mechanics

ISSN: 1735-3572    EISSN: 1735-3645


Prof. Ebrahim Shirani



Dr. Ahmad Reza Pishevar

Editorial Manager

Dr. Mohammad Reza Tavakoli

Secretary of JAFM

Mrs. Shakiba Rostami


JAFM is an open access, peer-reviewed online journal with a scope that covers all aspects of theoretical, numerical and experimental fluid mechanics. The emphasis is on the applied rather than purely mathematical aspects of fluid mechanics.


JAFM offers a rapid and high quality peer-review process overseen by its distinguished international Editorial Board. The journal benefits from an efficient online submission process and online publication upon acceptance.


JAFM papers are freely available and the accepted papers are published free of cost.


For further assistance for submitting manuscripts, the JAFM secretary may be contacted by the following email address:



Most Viewed Papers
Vol7 , No 2
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Title : A Novel Aerodynamic Design Method for Centrifugal Compressor Impeller
Pages : 329-344
Authors : M. Nili-Ahmadabadi,  mohammad durali,  Ali Hajilouy Benisi, 
Anstract : This paper describes a new quasi-3D design method for centrifugal compressor impeller. The method links up a novel inverse design algorithm, called Ball-Spine Algorithm (BSA), and a quasi-3D analysis. Euler equation is solved on the impeller meridional plane. The unknown boundaries (hub and shroud) of numerical domain are iteratively modified by BSA until a target pressure distribution in flow passage is reached. To validate the quasi-3D analysis code, existing compressor impeller is investigated experimentally. Comparison between the quasi-3D analysis and the experimental results shows good agreement. Also, a full 3D Navier-Stokes code is used to analyze the existing and designed compressor numerically. The results show that the momentum decrease near the shroud wall in the existing compressor is removed by hub-shroud modifications resulting an improvement in performance by 0.6 percent.