Shape Optimization of Nonplanar Lifting Surfaces and Planar–Nonplanar Break Points

Author:

Andrejašič Matej1,Veble Gregor1

Affiliation:

1. Research and Development Department, Pipistrel d.o.o. Ajdovščina, Ajdovščina SI-5270, Slovenia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference26 articles.

1. DRAG DUE TO LIFT: Concepts for Prediction and Reduction

2. ChambersJ. R. “Concept to Reality: Contributions of the NASA Langley Research Center to U.S. Civil Aircraft of the 1990s,” NASA SP-2003-4529, Oct. 2003, http://www.archive.org/details/nasa_techdoc_20030059513 [retrieved 2 Dec. 2011].

3. WhitcombR. T. “A Design Approach and Selected Wind-Tunnel Results at High Subsonic Mounted Speeds for Winglets,” NASA TN-D-8260, July 1976.

4. Design of Winglets for High-Performance Sailplanes

5. PrandtlL. “Applications of Modern Hydrodynamics to Aeronautics,” NACA TR-116, 1921.

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