Efficient Numerical Techniques for Simulating a Rotorcraft Flow Field with Overlapping Grids-Reference-Cited by-同舟云学术

Efficient Numerical Techniques for Simulating a Rotorcraft Flow Field with Overlapping Grids

Published:2015-05 Issue:5 Volume:53 Page:1372-1383
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Yang Xiaoquan¹,Yang Aiming²,Si Jiangtao¹

Affiliation:

1. General Configuration and Aerodynamics Department, Shanghai Aircraft Design and Research Institute, Commercial Aircraft Corporation of China, 201210 Shanghai, People’s Republic of China

2. Department of Mechanics and Engineering Science, Fudan University, 200433 Shanghai, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053426

Reference40 articles.

1. Helicopter rotor blade computation in unsteady flows using moving overset grids

2. Forward-Flight Analysis of Slatted Rotors Using Navier-Stokes Methods

3. Aeroelastic Analysis of Helicopter Rotor Blades on Deformable Chimera Grids

4. Navier-Stokes Analysis of Helicopter Rotor Aerodynamics in Hover and Forward Flight

5. Multigrid acceleration of an upwind Euler method for hovering rotor flows

Cited by 6 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. Aerodynamics and vibration analysis of a helicopter rotor blade;Acta Mechanica;2024-02-27

2. Experimental Study of Far-Field Aerodynamic Noise Characteristics of Serrated Slat;Journal of Aerospace Engineering;2023-01

3. Implicit Time-Spectral Method for Unsteady Reynolds-Averaged Navier–Stokes Computations of Turbulent Flows;AIAA Journal;2021-05

4. Effects of tip-jet on the performance of a ducted fan;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-09-13

5. Numerical investigations of ducted fan aerodynamic performance with tip-jet;Aerospace Science and Technology;2018-07