Bi-stable asymmetry on a pointed-nosed slender body at a high angle of attack
Author:
Affiliation:
1. Aircraft and Propulsion Laboratory, Ningbo Institute of Technology, Beihang University, Ningbo 315100, China
2. Ministry-of-Education Key Laboratory of Fluid Mechanics, Beihang University, Beijing 100191, China
Funder
National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0056494
Reference33 articles.
1. Influence of nose perturbations on behaviors of asymmetric vortices over slender body
2. Computational challenges in high angle of attack flow prediction
3. A physical model of asymmetric vortices flow structure in regular state over slender body at high angle of attack
4. Asymmetric vortices flow over slender body and its active control at high angle of attack
5. Recent progress on the study of asymmetric vortex flow over slender bodies
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