[PDF][PDF] 不同前倾角度倾转旋翼噪声数值计算分析
袁明川, 孙会迅, 李志彬, 牛青峰, 樊枫 - 西北工业大学学报, 2024 - scholar.archive.org
基于自由尾迹结合FW⁃ H (FfowcsWilliams⁃ Hawkings) 方程的方法建立了倾转旋翼气动噪声
计算模型, 并采用倾转旋翼模型噪声试验数据验证了计算分析方法的有效性. 选取典型过渡路径 …
计算模型, 并采用倾转旋翼模型噪声试验数据验证了计算分析方法的有效性. 选取典型过渡路径 …
Progress in Massively Parallel and Performance Portable Overset Implementations in HPCMP CREATE A/V Helios
J Sitaraman, S Hosseinverdi, D Jude, B Roget… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
This paper introduces a performance-portable approach for the dual-mesh overset
computational fluid dynamics paradigm used in the high fidelity DoD HPCMP CREATE …
computational fluid dynamics paradigm used in the high fidelity DoD HPCMP CREATE …
[PDF][PDF] Aeroelastic Load Evaluation During Tiltrotor Transition Using a Comprehensive Mid-Fidelity Approach
This study examines the aeromechanics of tiltrotor conversion maneuvers using a coupled
simulation approach, integrating the multibody dynamics code MBDyn with the mid-fidelity …
simulation approach, integrating the multibody dynamics code MBDyn with the mid-fidelity …
Numerical calculation and analysis of aero-acoustic characteristics of tilt rotor in different tilt angles
Y Mingchuan, SUN Huixun, LI Zhibin… - Xibei Gongye Daxue …, 2024 - jnwpu.org
The numerical calculation model for the aero-acoustic analysis of a tilt rotor was established
by combining the free wake method and the FW-H (Ffowcs Williams-Hawkings) equation …
by combining the free wake method and the FW-H (Ffowcs Williams-Hawkings) equation …
Active Vibration Control Using Electric Rotor Torques In eVTOL Aircraft
C Cho - 2024 - etda.libraries.psu.edu
Electric aircraft are attracting more interest in both commercial and military markets due to
their distinctive advantages, including environmental friendliness and reduced maintenance …
their distinctive advantages, including environmental friendliness and reduced maintenance …
[PDF][PDF] Experimental and Computational Investigations of Propeller–Wing Interactions for Varying Propeller Tilt Angles
ABSTRACT A joint experimental-computational research campaign is underway to develop
physical understanding and a validation-quality database for a model-scale tractor propeller …
physical understanding and a validation-quality database for a model-scale tractor propeller …
Wind Tunnel Measurements On The Effect of Propeller Tilt On Propeller--Wing Interactional Aerodynamics
S Srivathsan, J Rauleder - AIAA AVIATION FORUM AND ASCEND …, 2024 - arc.aiaa.org
Advancements in technology over the last decade have led to a rise in the popularity of
electric-powered aircraft for a range of vertical take-off and landing urban and advanced air …
electric-powered aircraft for a range of vertical take-off and landing urban and advanced air …
[PDF][PDF] Active Vibration Damping and Harmonic Vibration Reduction in an eVTOL Aircraft Model Using Electric Rotor Torque
Rotorcraft experience significant vibrations due to periodic aerodynamic forces and
moments on the rotor blades and wings. Rotor torque damping is a novel vibration damping …
moments on the rotor blades and wings. Rotor torque damping is a novel vibration damping …