Design and Evaluation of Aeroelastically Tuned Joined-Wing SensorCraft Flight Test Article-Reference-Cited by-同舟云学术

Design and Evaluation of Aeroelastically Tuned Joined-Wing SensorCraft Flight Test Article

Published:2013-04-05 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Richards Jenner¹,Garnand-Royo Jeffrey S.²,Suleman Afzal¹,Canfield Robert A.²,Woolsey Craig A.²

Affiliation:

1. University of Victoria

2. Virginia Polytechnic Institute and State University

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. Joined-Wing Aeroelastic Design with Geometric Nonlinearity

2. 2Bond, V., Flexible Twist for Pitch Control in a High Altitude Long Endurance Aircraft with Nonlinear Response, Ph.D. Dissertation Prospectus, Department of the Air Force,Air Force Institute of Technology, Wright-Patterson AFB, Dayton, OH,2007.

3. 3The Boeing Company. Selected Results from Test of Model on Sting, Presentation Excerpts, NASA Langley, Hampton VA, slides 2-5.

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Ground Servoelasticity Test and Analysis of UAVs With Large Aspect Ratio and Joined-Wing Layout;IEEE Access;2024

2. Study of Effect of Aerodynamic Interference on Transonic Flutter Characteristics of Airfoil;AIAA Journal;2023-11-02

3. Aeroelastic Optimization Design of the Global Stiffness for a Joined Wing Aircraft;Applied Sciences;2021-12-12

4. Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future;Progress in Aerospace Sciences;2016-11

5. Buckling Alleviation for Joined-Wing Aircraft;Journal of Aircraft;2016-05