Pressure Sensitive Paint Measurements on 15% Scale Rotor Blades in Hover-Reference-Cited by-同舟云学术

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Pressure Sensitive Paint Measurements on 15% Scale Rotor Blades in Hover

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Fluid Dynamics Conference and Exhibit
language:
Short-container-title:

Author:

Wong Oliver¹,Watkins A.²,Ingram JoAnne³

Affiliation:

1. U.S. Army

2. NASA Langley Research Center

3. Swales Aerospace

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-5008

Reference28 articles.

1. Measurement Around a Rotor Blade Excited in Pitch, Part 2: Unsteady Surface Pressure

Cited by 13 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. Fast-Responding Pressure-Sensitive Paint Measurements of the IC3X at Mach 7.2;Aerospace;2023-10-18

2. Implementation of an Unsteady PSP System in the NASA Transonic Dynamics Tunnel;AIAA AVIATION 2022 Forum;2022-06-20

3. A Lifetime-PSP Study of Dynamic Stall on Pitching Swept Finite-Aspect-Ratio Wings;AIAA SCITECH 2022 Forum;2022-01-03

4. Fast pressure-sensitive paint for understanding complex flows: from regular to harsh environments;Experiments in Fluids;2019-11-23

5. Review of measurement techniques for unsteady helicopter rotor flows;Progress in Aerospace Sciences;2019-11

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