Low-Reynolds Number Behavior of the Leading-Edge Suction Parameter at Low Pitch Rates-Reference-Cited by-同舟云学术

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Low-Reynolds Number Behavior of the Leading-Edge Suction Parameter at Low Pitch Rates

Published:2021-09-16 Issue: Volume: Page:1-9
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Kay Nicholas J.¹^ORCID,Richards Peter J.¹,Sharma Rajnish N.¹

Affiliation:

1. University of Auckland, Auckland 1023, New Zealand

Funder

The University of Auckland

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060733

Reference34 articles.

1. AustinR., Unmanned Aircraft Systems: UAVS Design, Development, and Deployment, Wiley, West Sussex, U.K., 2010, pp. 1–15, Chap. 1.

2. Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications

3. Challenges Facing Future Micro-Air-Vehicle Development

4. FahlstromP.GleasonT., Introduction to UAV Systems, Wiley, West Sussex, U.K., 2012, pp. 17–31, Chap. 2.

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4. Prediction of Vortex Initiation using an Unsteady Panel Method with an Integral-Boundary-Layer Calculation;AIAA AVIATION 2022 Forum;2022-06-20

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