Exploratory Wind Tunnel Gust Alleviation Tests of a Multiple-Flap Flexible Wing-Reference-Cited by-同舟云学术

Exploratory Wind Tunnel Gust Alleviation Tests of a Multiple-Flap Flexible Wing

Published:2022-01-03 Issue: Volume: Page:
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Container-title:AIAA SCITECH 2022 Forum
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Author:

Berg John¹,Ting Kuang-Ying¹,Mundt Tyler J.¹,Mor Marat¹,Livne Eli¹,Morgansen Kristi A.¹

Affiliation:

1. University of Washington

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2488

Reference28 articles.

1. A wind-tunnel technique for measuring frequency-response functions for gust load analyses.

2. Buell, D. A. "An Experimental Investigation of the Velocity Fluctuations Behind Oscillating Vanes," Tech. Rep. TN D-5543, NASA, Nov. 1969.

3. A Wind-Tunnel Stream Oscillation Apparatus

4. Ham, N. D., Bauer, P. H., and Lawrence, T. L. "Wind Tunnel Generation of Sinusoidal Lateral and Longitudinal Gusts by Circulation of Twin Parallel Airfoils," Tech. Rep. CR 137547, ASRL TR 174-3, NASA, Aug. 1974.

5. Experiments and analysis for a gust generator in a wind tunnel

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