CFD of NACA airfoil with passage

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• Published Subscription 4 Jul 2015

  CFD Analysis of NACA 2412 and NACA 2412 with Passage for Lift Augmentation

  By Sanjay N. Havaldar, Shardul Pawar, Apoorva Lele, Aniket Rishi, Rahul Pradhan

  Abstract: Computational Fluid Dynamics (CFD) analysis of a three dimensional (3-D) National Advisory Committee for Aeronautics (NACA) 2412 airfoil was compared with same dimensional 3-D NACA 2412 with internal passage. The computational domain was composed of 2109509 elements for NACA 2412 and 2258962 elements for NACA 2412 with internal passage. Calculations were done for various Mach numbers by varying the angle of attack constant for above mentioned turbulence model. The flow …

  Published in Journal of Aerospace Engineering & Technology · Vol. 5, Issue 2, 2015 · pp. 1–7 Read article →