Structural control of asymmetric forebody vortices over a slender body
Author:
Affiliation:
1. Ministry-of-Education Key Laboratory of Fluid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
2. Aircraft and Propulsion Laboratory, Ningbo Institute of Technology, Beihang University, Ningbo 315800, China
Funder
National Natural Science Foundation of China
Ningbo National Natural Science Foundation
Research Fund of Key Laboratory of Unsteady Aerodynamics and Flow Control
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0068576
Reference35 articles.
1. Proportional Control of Asymmetric Forebody Vortices
2. Fluid-structure interaction of a rolling restrained body of revolution at high angles of attack
3. Recent progress on the study of asymmetric vortex flow over slender bodies
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1. The influence of roll angles on unsteady aerodynamics in a canard‐configured missile;International Journal of Mechanical System Dynamics;2024-05-14
2. Evolution and Influence of Multivortex Structure on the Head of Canard‐Controlled Missile at High Angle of Attack;International Journal of Aerospace Engineering;2024-01
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