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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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
Vol8 , No 1
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Title : Numerical Aerodynamic Evaluation and Noise Investigation of a Bladeless Fan
Pages : 133-142
Authors : mohammad jafari,  Hossein Afshin,  Bijan Farhanieh,  Hamidreza bozorgasareh, 
Anstract : Bladeless fan is a novel fan type that has no observable impeller, usually used for domestic applications. Numerical investigation of a Bladeless fan via Finite Volume Method was carried out in this study. The fan was placed in center of a 4×2×2m room and 473 Eppler airfoil profile was used as cross section of the fan. Performance and noise level of the fan by solving continuity and momentum equations as well as noise equations of Broadband Noise Source (BNS) and Ffowcs Williams and Hawkings (FW-H) in both steady state and unsteady conditions were studied. Flow increase ratio of the fan was captured. Furthermore, BNS method could find outlet slit of the air as the main source of the noise generation. In order to validation of aeroacousticcode results, a simulation of noise for NACA 0012 airfoil via FW-H method was compared to experimental results and good agreement was obtained.