Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations-Reference-Cited by-同舟云学术

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Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations

Published:2013-03 Issue:2 Volume:50 Page:378-387
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Zhang G. Q.¹,Yu S. C. M.¹,Chien A.²,Yang S. X.³

Affiliation:

1. Aerospace Engineering Division, Nanyang Technological University, Singapore 639798, Republic of Singapore

2. Department of Radiological Sciences, University of California, Los Angeles, California 90095

3. Aircraft Design Division, Beijing Institute of Technology, 100081 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031740

Reference16 articles.

1. Vortex-wing interaction of a close-coupled canard configuration

2. Flowfield study of a close-coupled canard configuration

3. Rotor Design for the Performance Optimization of Canard Rotor/Wing Aircraft

4. Effect of canard stall on projectile roll and pitch damping

5. Hub Drag-Reduction Strategies of Canard Rotor/Wing Unmanned Aerial Vehicles

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1. Characteristics of Vortices around Forward Swept Wing at Low Speeds/High Angles of Attack;Aerospace;2023-09-08

2. Design and Analysis of Wing Tip Twist on a Forward Swept Wing Using Prandtl-d Wing Concept;Journal of Aerospace Sciences and Technologies;2023-07-26

3. Supersonic Forward-Swept Wing Design Using Multifidelity Efficient Global Optimization;Journal of Aircraft;2022-07

4. Unconventional aircraft for civil aviation: A review of concepts and design methodologies;Progress in Aerospace Sciences;2022-05

5. A Slider-Type Trim Strategy to Deal with Wing Perforation Damage Based on CFD;Lecture Notes in Electrical Engineering;2021-11-02

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