Design and Testing of a Multi-Element Airfoil for Short-Takeoff-and-Landing Ultralight Aircraft
Author:
Affiliation:
1. University of Naples “Federico II”, 80125 Napoli, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.43429
Reference19 articles.
1. Design of a Low-Cost Easy-to-Fly STOL Ultralight Aircraft in Composite Material
2. Parametric Investigation of a High-Lift Airfoil at High Reynolds Numbers
3. High Reynolds Number, Multielement Airfoil Flowfield Measurements
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