Author: Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
EXPERIMENTAL STUDY OF LIFT-ENHANCING TABS ON A TWO-ELEMENT AIRFOIL... NASA/TM-95-207303... MAY 5, 1998
Author: Experimental and Computational Investigation of Lift-enhancing Tabs ... Nasa-tm-110432 ... National Aeronautic
Author: EXPERIMENTAL STUDY OF SADDLE POINT OF ATTACHMENT IN LAMINAR JUNCTURE FLOW... NASA/TM-95-207302... AUG. 6, 1998
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Static Extended Trailing Edge for Lift Enhancement: Experimental and Computational Studies
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
A static extended trailing edge attached to a NACA0012 airfoil section is studied for achieving lift enhancement at a small drag penalty. It is indicated that the thin extended trailing edge can enhance the lift while the zero-lift drag is not significantly increased. Experiments and calculations are conducted to compare the aerodynamic characteristics of the extended trailing edge with those of Gurney flap and conventional flap. The extended trailing edge, as a simple mechanical device added on a wing without altering the basic configuration, has a good potential to improve the cruise flight efficiency.