A Fast Approach to Model the Effects of Propeller Slipstream on Wing Load Distribution-Reference-Cited by-同舟云学术

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A Fast Approach to Model the Effects of Propeller Slipstream on Wing Load Distribution

Published:2015-01-02 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Agostinelli Christian¹,Simeone Simone¹,Rampurawala Abdul²,Allen Christian B.¹,Zhu Feng³

Affiliation:

1. University of Bristol

2. Airbus

3. University of Sheffield

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0028

Reference25 articles.

1. A perspective on computational algorithms for aerodynamic analysis and design

2. Flexible Wing Twist Optimisation using Rapid Computational Methods

3. A Rapid Approach to the Aerodynamic Design of a Flexible High-Lift Wing

Cited by 3 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. The Aerodynamics and Hover Control for the X-wing VTOL MAV;Proceedings of 2021 International Conference on Autonomous Unmanned Systems (ICAUS 2021);2022

2. Research on Design Domain of Propeller-Driven Hybrid-Mode Aerial Vehicle;18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2017-06-02

3. Research on Design Domain of Propeller-Driven Hybrid-Mode Aerial Vehicle;16th AIAA Aviation Technology, Integration, and Operations Conference;2016-06-10

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