[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 …

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 …

[PDF][PDF] Aeroelastic Load Evaluation During Tiltrotor Transition Using a Comprehensive Mid-Fidelity Approach

A Cocco, U Saetti, A Savino - 50th European Rotorcraft Forum …, 2024 - researchgate.net
This study examines the aeromechanics of tiltrotor conversion maneuvers using a coupled
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 …

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 …

[PDF][PDF] Experimental and Computational Investigations of Propeller–Wing Interactions for Varying Propeller Tilt Angles

S Srivathsan, P Sridhar, MJ Smith, J Rauleder - 2024 - researchgate.net
ABSTRACT A joint experimental-computational research campaign is underway to develop
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 …

[PDF][PDF] Active Vibration Damping and Harmonic Vibration Reduction in an eVTOL Aircraft Model Using Electric Rotor Torque

C Cho, CD Rahn, E Smith, P Singh - 2024 - researchgate.net
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 …