Fundamental Solutions of the Potential Flow Equations for Rotorcraft with Applications-Reference-Cited by-同舟云学术

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Fundamental Solutions of the Potential Flow Equations for Rotorcraft with Applications

Published:2015-05 Issue:5 Volume:53 Page:1251-1261
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Fei Zhongyang¹,Peters David A.²

Affiliation:

1. Department of Control Science & Engineering, Harbin Institute of Technology, Harbin, 150001 Heilongjiang, People’s Republic of China

2. Department of Mechanical Engineering & Materials Science, Washington University in St. Louis, St. Louis, MI 63130

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053308

Reference21 articles.

1. The Free Wake Analysis

2. An Analytical Method for Predicting Rotor Wake Geometry

3. Rotor Free‐Wake Modeling Using a Pseudo‐Implicit Technique — Including Comparisons with Experimental Data

4. Free-wake analysis of compressible rotor flows

5. Conservative full-potential model for unsteady transonic rotor flows

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1. Considerations in the Selection of Inflow States with Finite-State Dynamic Inflow;AIAA Journal;2021-07

2. Field investigation and full-scale model testing of mud pumping and its effect on the dynamic properties of the slab track–subgrade interface;Proceedings of the Institution of Mechanical Engineers, Part F: Journal of Rail and Rapid Transit;2018-11-12

3. Event driven tracking control algorithm for marine vessel based on backstepping method;Neurocomputing;2016-09

4. Three-dimensional dynamic inflow below the rotor disk based on the finite-state method;Journal of Vibration and Control;2016-08-08

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