Effects of Reynolds Number on Flow over 76/40-Degree Double-Delta Wings
Author:
Affiliation:
1. Delft University of Technology, 2600 GB Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3033
Reference11 articles.
1. A numerical investigation of vortex flow control through small geometry modifications at the strake/wing junction of a cropped double-delta wing
2. Upwind Navier-Stokes solutions for leading-edge vortex flows
3. Numerical investigation of high incidence flow over a double-delta wing
4. A study of the vortex flow over a 76/40-deg double-delta wing
5. Reynolds number effects on the vortical-flow structure generated by a double-delta wing
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