Prediction of Noise from Low Reynolds Number Rotors with Different Number of Blades using a Non-Linear Vortex Lattice Method-Reference-Cited by-同舟云学术

Prediction of Noise from Low Reynolds Number Rotors with Different Number of Blades using a Non-Linear Vortex Lattice Method

Published:2019-05-18 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Jo Yeongmin¹,Jardin Thierry¹,Gojon Romain¹,Jacob Marc C.¹,Moschetta Jean-Marc¹

Affiliation:

1. Higher Institute of Aeronautics and Space (ISAE-SUPAERO)

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. Kunz, P. J. “Aerodynamics and Design for Ultra-Low Reynolds Number Flight,” Ph.D. Dissertation,Stanford University, 2003.

2. Bohorquez, F. “Rotor Hover Performance and System Design of An Efficient Coaxial Rotary Wing Micro Air Vehicle,” Ph.D. Dissertation,University of Maryland, College Park, 2007.

Cited by 21 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A multivariate and wavelet-based analysis on the wall pressure fluctuations for propellers in ground effect;International Journal of Aeroacoustics;2024-09-08

2. Experimental Validation of Vortex Particle Method for Modeling of Rotor Interaction Noise;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

3. LBM and iLES Comparison for the Aaerodynamic and Acoustic Characteristics of a Low-speed Rotor;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

4. Large-Eddy Simulations of a Rotor With Impedance Patches on Its Blades;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

5. Analysis of MAV Rotors Optimized for Low Noise and Aerodynamic Efficiency with Operational Constraints;Fluids;2024-04-19