An Approach to Induced Drag Reduction and its Experimental Evaluation

Author:

Eller David,Heinze Sebastian

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Adaptive wing and flow control technology

2. Design concept of a high-altitude long-endurance unmanned aerial vehicle

3. J. Simpson, J. Schweiger, and S. Kuzmina. Design of an adaptive wing shape control concept for minimum induced drag of a transport aircraft. InCEAS/AIAA/NvVL International Forum for Aeroelasticity and Structural Dynamics, Amsterdam, 2003.

4. Aeroelastic Wing with Leading- and Trailing-Edge Control Surfaces

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