Hysteresis and Broad Flow Features on a Swept Wing at High Lift
Author:
Affiliation:
1. National Aerospace Laboratories, Bangalore 560 017, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.17397
Reference16 articles.
1. The aerodynamic design of multi-element high-lift systems for transport airplanes
2. In-Flight Boundary-Layer State Measurements on a High-Lift System: Main Element and Flap
3. Separation control on high-lift airfoils via micro-vortex generators
4. Experimental investigation of the confluent boundary layer of a multielement low speed airfoil
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