Leading-Edge Radius Effects on Aerodynamic Characteristics of 50-Degree Delta Wings
Author:
Affiliation:
1. Delft University of Technology, Delft 2600 GB, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031550
Reference25 articles.
1. Unsteady aerodynamics of nonslender delta wings
2. Compact Difference Scheme Applied to Simulation of Low-Sweep Delta Wing Flow.
3. Chen, L., and Wang, J. J. "Numerical Simulations of Leading-Edge Vortex Core Axial Velocity for Flow over Delta Wings," Science in pp. 2029-2036. doi:10.1007/s11431-009-0082-8
4. An Investigation of Vortex Flows over Low Sweep Delta Wings
5. Experimental Investigations on Leading-Edge Vortex Structures for Flow over Non-Slender Delta Wings
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