Application of airfoil theory for nonuniform streams to wing propeller interaction.
Author:
Affiliation:
1. New York University, Bronx, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44327
Reference12 articles.
1. Thin airfoil in nonuniform parallel streams.
2. Numerical investigations of an airfoil in a nonuniform stream
3. Airfoils in Two-Dimensional Nommiformly Sheared Slipstreams
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3. Quasi-steady aerodynamic analysis of propeller-wing interaction;International Journal for Numerical Methods in Fluids;1999-08-30
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