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Efficient Simulation Method for Helicopter Rotor/Horizontal Tail Aerodynamic Interference Based on High-Fidelity Reduced-Order Modeling
Yu Xi LIU renliang chen
Acta Aeronautica et Astronautica Sinica . 0, (): 1 -0 .  DOI: 10.7527/S1000-6893.2026.33384

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341