Study on the Influence of Mass Flow Rate over a National Advisory Committee for Aeronautics 6321 Airfoil Using Improved Blowing and Suction System for Effective Boundary Layer Control

• Published in: SAE International journal of aerospace Vol. 14; no. 2; pp. 219 - 233
• Main Authors: Karuppiah, Balaji, Wessley, Jims John
• Format: Journal Article
• Language: English
• Published: Warrendale SAE International 01.12.2021; SAE International, a Pennsylvania Not-for Profit
• Subjects: Aerodynamic coefficients; Aerodynamic efficiency; Aerodynamics; Aeronautics; Airfoils; Angle of attack; Blowing rate; Boundary layer control; Control systems; Flow control; Improved blowing and suction system (IBSS); Mach number; Mass flow rate; NACA 6321; Numerical analysis; Reynolds averaged Navier-Stokes method; Stalling; Stalling angle; Suction; Three dimensional analysis; Three dimensional flow; Wings (aircraft)

The numerical analysis of the three-dimensional (3D) flow over a National Advisory Committee for Aeronautics (NACA) 6321 airfoil to evaluate the mass flow rate by using a novel method Improved Blowing and Suction System (IBSS) to control the boundary layer is presented in this study. Analysis is per...