High-Lift Propulsive Airfoil with Integrated Crossflow Fan
Author:
Affiliation:
1. Syracuse University, Syracuse, New York 13244
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.17610
Reference18 articles.
1. On Cross-Flow Fan Similarity: Effects of Casing Shape
2. Wake ingestion propulsion benefit
3. Thick-wing spanloader all-freighter - A design concept for tomorrow's air cargo
4. Ko, Y.Y. A. "The Multidisciplinary Design Optimization of a Distributed Propulsion Blended-Wing-Body Aircraft," Ph.D. Dissertation,Virginia Polytechnic Institute and State University, Blacksburg, VA, 2003.
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