Method of Characteristics Analysis of Open-Return, Unsteady-Flow Wind-Tunnel Performance
Author:
Affiliation:
1. University of Notre Dame, Notre Dame, Indiana, 46545
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061751
Reference18 articles.
1. WilliamsD. R.StasseQ.RennieR. M. “Lift, Drag, and Moment Response of a UCAS Model Experiencing Longitudinal von Karman Gust Spectra,” AIAA Paper 2019-1149, Jan. 2019. 10.2514/6.2019-1149
2. GloutakD. A.CostantinoE.FarnsworthJ. A. N. “Characteristic Wing Measurements of a NACA 0015 in Steady and Unsteady Surging Wind Tunnel Flow,” AIAA Paper 2020-1558, Jan. 2020. 10.2514/6.2020-1558
3. An experimental investigation into the influence of unsteady wind on the performance of a vertical axis wind turbine
4. Challenges Facing Future Micro-Air-Vehicle Development
5. Lift-Enhancing Vortex Flows Generated by Plunging Rectangular Wings with Small Amplitude
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1. Unsteady Pressure Gradients in Wind Tunnels with Time-Varying Freestreams;AIAA Journal;2024-07-15
2. Measurement and Modeling of Subscale Open-Return Unsteady Wind-Tunnel Behavior;AIAA Journal;2024-07-02
3. Measurement and Modeling of Subscale Open-Return Unsteady Wind-Tunnel Behavior;AIAA SCITECH 2024 Forum;2024-01-04
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