Effect of changes in flap deflection and addition of slat clearance on aerodynamic performance of the wing airfoil NACA 43018 in the cruising and landing phases
Author:
Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0115108
Reference11 articles.
1. Influence of a slotted flap gap size on the aerodynamic characteristics of a light aircraft wing at taking off and landing
2. Effect of the Slot Span on the Wing Performance
3. Control of Separation on the Flap of a Three-Element High-Lift Configuration
4. Comparative Study of Forward Wingtip Fence and Rearward Wingtip Fence on Wing Airfoil Eppler E562
5. E.N. Jacobs and I.H. Abbot (1939). Airfoil Section Data Obtained in the NACA Variable-Density Tunnel as Affected by Support Interference and other Correction. In National Advisory Committee For Aeronautics (Issue 669).
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