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WIND TUNNEL RESEARCH ON THE INFLUENCE OF ACTIVE AIRFLOW ON THE LIFT FORCE GENERATED BY THE AIRFOIL
2013
Advances in Science and Technology Research Journal
The paper discusses the results of wind tunnel tests of airfoils with additional active airflow applied to their upper surfaces. These studies were carried out for a range of velocities up to 28 m/s in an open wind tunnel. Several types of airfoils selected for the examination feature different geometries and are widely applied in today's aviation industry. The changes in the lift and drag force generated by these airfoils were recorded during the study. The test bench for the tests was
doi:10.5604/20804075.1062366
fatcat:r7vdhjzrajfwddjzjaekib7q2u