Numerical Investigation of Engine Effects on a Transport Aircraft with Circulation Control
Author:
Affiliation:
1. Transport Aircraft Branch, Institute of Aerodynamics and Flow Technology, DLR, German Aerospace Center, 38108 Braunschweig, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032724
Reference19 articles.
1. Aerodynamics of Powered High-Lift Systems
2. Recent Experimental Development of Circulation Control Airfoils and Pneumatic Powered-Lift Systems
3. Overview of Recent Circulation Control Modeling Activities at Cal Poly
4. Numerical Approach Aspects for the Investigation of the Longitudinal Static Stability of a Transport Aircraft with Circulation Control
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