Stochastic Investigation on the Robustness of Laminar-Flow Wings for Flight Tests-Reference-Cited by-同舟云学术

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Stochastic Investigation on the Robustness of Laminar-Flow Wings for Flight Tests

Published:2022-04 Issue:4 Volume:60 Page:2266-2286
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Yang Tihao¹,Chen Yifu¹,Shi Yayun²^ORCID,Hua Jun³,Qin Feifei⁴,Bai Junqiang¹

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, Shaanxi, People’s Republic of China

2. Xi’an Jiaotong University, 710072 Xi’an, Shaanxi, People’s Republic of China

3. Chinese Aeronautical Establishment, 100012 Beijing, People’s Republic of China

4. Swiss Federal Institute of Technology, 8093 Zürich, Switzerland

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.J060842

Reference27 articles.

1. Review of hybrid laminar flow control systems

2. Sensitivity of high-speed boundary-layer stability to base-flow distortion

3. Design and Test of the UW-5006 Transonic Natural-Laminar-Flow Wing

4. Efficient Aerodynamic Shape Optimization with Deep-Learning-Based Geometric Filtering

5. Correction: Nonlinear Theoretical Aeroelastic Model of a Plate: Free to Fixed In-Plane Boundaries

Cited by 4 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. Aerostructural Optimization and Comparative Study of Twin-Fuselage and Strut-Braced-Wing Aircraft Configurations;Journal of Aircraft;2023-12-09

2. Complex Standard Eigenvalue Problem Derivative Computation for Laminar–Turbulent Transition Prediction;AIAA Journal;2023-08

3. Uncertainty Quantification and Sensitivity Analysis of Closure Parameters of Transition Models;Journal of Aerospace Engineering;2023-01

4. Geometrically Nonlinear Coupled Adjoint Aerostructural Optimization of Natural-Laminar-Flow Strut-Braced Wing;Journal of Aircraft;2022-12-18

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