Validation of the Steady-State Hover Formulation for Accurate Performance Predictions-Reference-Cited by-同舟云学术

Validation of the Steady-State Hover Formulation for Accurate Performance Predictions

Published:2019-12 Issue:12 Volume:57 Page:5293-5308
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Fitzgibbon T. A.¹,Woodgate M. A.¹,Jimenez-Garcia A.¹,Barakos G. N.¹

Affiliation:

1. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom

Funder

Defence Science and Technology Laboratory

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference49 articles.

1. JohnsonC. “Optimisation of Aspects of Rotor Blades Using Computational Fluid Dynamics,” Ph.D. Thesis, Univ. of Liverpool, Liverpool, England, U.K. 2012.

2. A review of helicopter rotor blade tip shapes

3. The Wake Geometry of a Hovering Helicopter Rotor and Its Influence on Rotor Performance

4. A Prescribed Wake Lifting Surface Hover Performance Analysis

Cited by 5 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. Aeroelastic fluid dynamics assessment of performance and vibration on active twisting rotors;Aerospace Science and Technology;2024-08

2. Numerical simulation of distributed propulsion systems using CFD;Aerospace Science and Technology;2024-04

3. Numerical Analysis of HVAB and STAR Rotor Blades Using HMB3;AIAA SCITECH 2023 Forum;2023-01-19

4. Blade tip geometry effect on the aerodynamic performance of a low-speed Rim Driven Thruster;AIAA AVIATION 2022 Forum;2022-06-20

5. Investigation of Wake Breakdown in Hover Using The HMB3 Solver;AIAA SCITECH 2022 Forum;2022-01-03