Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig-Reference-Cited by-同舟云学术

Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig

Published:2019-05 Issue:3 Volume:56 Page:1029-1039
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Gong Z.¹,Araujo-Estrada S.²,Lowenberg M. H.²,Neild S. A.²,Goman M. G.³

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, Nanjing 210016, People’s Republic of China

2. University of Bristol, Bristol, England BS8 1TR, United Kingdom

3. De Montfort University, Leicester, England LE1 9BH, United Kingdom

Funder

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034995

Reference18 articles.

1. Anon. “Cooperative Programme on Dynamic Wind Tunnel Experiments for Manoeuvring Aircraft,” AGARD-AR-305, 1996.

2. ChambersJ. R. “Modeling Flight: The Role of Dynamically Scaled Free-Flight Models in Support of NASA’s Aerospace Programs,” NASA SP 2009-575, 2009.

3. Overview of Dynamic Test Techniques for Flight Dynamics Research at NASA LaRC

4. A Review of Wind Tunnel Based Virtual Flight Testing Techniques for Evaluation of Flight Control Systems

5. Dynamic Rig for Validation of Control Algorithms at High Angles of Attack

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