Vortex Oscillations Around a Hemisphere-Cylinder Body with a High Fineness Ratio
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
Funder
the National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056047
Reference55 articles.
1. Asymmetric Vortices on a Slender Body of Revolution
2. Pressures Around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent Separation
3. Proportional Control of Asymmetric Forebody Vortices
4. Influence of nose perturbations on behaviors of asymmetric vortices over slender body
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