Numerical Simulation of Plunging Wing Section at High Angles of Attack
Author:
Affiliation:
1. New Mexico State University, Las Cruces, New Mexico 88003
2. University of Arizona, Tucson, Arizona 85721
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J056763
Reference26 articles.
1. Current and Future Research in Active Control of Lightweight, Flexible Structures Using the X-56 Aircraft
2. Oscillation Frequency and Amplitude Effects on the Wake of a Plunging Airfoil
3. Vortex Lock-In Phenomenon in the Wake of a Plunging Airfoil
4. High-Fidelity Simulation of Transitional Flows past a Plunging Airfoil
5. Numerical Investigation of Deep Dynamic Stall of a Plunging Airfoil
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