Overview of Low Speed Wind Tunnel Testing Conducted on a Wingtip Mounted Propeller for the Workshop for Integrated Propeller Prediction-Reference-Cited by-同舟云学术

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Overview of Low Speed Wind Tunnel Testing Conducted on a Wingtip Mounted Propeller for the Workshop for Integrated Propeller Prediction

Published:2020-06-08 Issue: Volume: Page:
ISSN:
Container-title:AIAA AVIATION 2020 FORUM
language:
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Author:

Hooker John R.¹,Wick Andrew¹,Ginn Starr R.²,Walker Jimmy¹,Schiltgen Benjamin T.³

Affiliation:

1. Helden Aerospace

2. NASA Armstrong Flight Research Center

3. Empirical Systems Aerospace, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Reference2 articles.

Cited by 10 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. Wind tunnel test of full-scale wing-propeller system of a eVTOL aircraft;The Aeronautical Journal;2023-12-12

2. Contribution of Swirl Recovery to the Induced Drag of a Propeller-Wing System – A Parametric Study;AIAA AVIATION 2023 Forum;2023-06-08

3. Dual-Solver Hybrid Computational Approach to Integrated Propulsion Aerodynamics;Journal of Aircraft;2023-03

4. Numerical Simulation of Distributed Propulsion Systems Using Cfd;2023

5. Numerical Analysis of Propeller Mounting Position Effects on Aerodynamic Propeller/Wing Interaction;AIAA SCITECH 2022 Forum;2022-01-03

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