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Information Journal Paper

Title

EXPERIMENTAL INVESTIGATION ON THE AERODYNAMIC PERFORMANCE OF NLF-0414 ICED-AIRFOIL

Pages

  587-592

Abstract

 Icing phenomenon on a NATURAL LAMINAR FLOW AIRFOIL (NLF-0414) has been experimentally investigated.Double horn glaze ice geometry which was acquired during a 15 minutes spray time at−2.23oC with liquid water content and a median volumetric diameter of 1.0 g/m3 and 20 mm, has been extracted from database of NASA Lewis Research Center. Pressure distribution over airfoil surfacewas evaluated at angles of attack between -2 to 6 degreesfor both iced and clean airfoils. AERODYNAMICS PERFORMANCE degradation of the iced airfoil has been studied and it is shown that DOUBLE HORN ICE accretion, due to its unique geometry, severely affects aerodynamic characteristics of NATURAL LAMINAR FLOW AIRFOILs. Reattachment locations have been evaluated for upper and lower separation bubbles. The upper surface separation bubble was seen to increase in size in contrary to the lower surface separation bubble.

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  • Cite

    APA: Copy

    EBRAHIMI, A., HAJIPOUR, M., & HASHEMINASAB, H.. (2016). EXPERIMENTAL INVESTIGATION ON THE AERODYNAMIC PERFORMANCE OF NLF-0414 ICED-AIRFOIL. JOURNAL OF APPLIED FLUID MECHANICS (JAFM), 9(2), 587-592. SID. https://sid.ir/paper/307648/en

    Vancouver: Copy

    EBRAHIMI A., HAJIPOUR M., HASHEMINASAB H.. EXPERIMENTAL INVESTIGATION ON THE AERODYNAMIC PERFORMANCE OF NLF-0414 ICED-AIRFOIL. JOURNAL OF APPLIED FLUID MECHANICS (JAFM)[Internet]. 2016;9(2):587-592. Available from: https://sid.ir/paper/307648/en

    IEEE: Copy

    A. EBRAHIMI, M. HAJIPOUR, and H. HASHEMINASAB, “EXPERIMENTAL INVESTIGATION ON THE AERODYNAMIC PERFORMANCE OF NLF-0414 ICED-AIRFOIL,” JOURNAL OF APPLIED FLUID MECHANICS (JAFM), vol. 9, no. 2, pp. 587–592, 2016, [Online]. Available: https://sid.ir/paper/307648/en

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