Transition Prediction for Hybrid Laminar Flow Control Flight Test Considering Geometric Uncertainties-Reference-Cited by-同舟云学术

Transition Prediction for Hybrid Laminar Flow Control Flight Test Considering Geometric Uncertainties

Published:2022-11 Issue:6 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yang Tihao¹,Wang Yiwen²,Shi Yayun³^ORCID,Bai Junqiang⁴,Zhong Hai⁵,Wang Meng⁶

Affiliation:

1. Assistant Research Fellow, School of Aeronautics, Northwestern Polytechnical Univ., 127 West Youyi Rd., Beilin District, Xi’an, Shaanxi 710072, PR China.

2. Unmanned System Research Institute, Northwestern Polytechnical Univ., 127 West Youyi Rd., Beilin District, Xi’an, Shaanxi 710072, PR China.

3. Assistant Professor, School of Aerospace Engineering, Xi’an JiaoTong Univ., No. 28 Xianning West Rd., Xi’an, Shaanxi 710049, PR China (corresponding author). ORCID: .

4. Professor, School of Aeronautics, Northwestern Polytechnical Univ., 127 West Youyi Rd., Beilin District, Xi’an, Shaanxi 710072, PR China.

5. Senior Engineer, Aircraft Flight Test Technology Institute, Chinese Flight Test Establishment, 5 Lingyun Rd., Yanliang District, Xi’an, Shaanxi 710089, PR China.

6. Senior Engineer, Key Laboratory of Flow Visualization and Measurement Techniques, AVIC Aerodynamics Research Institute, Shenyang, Liaoning 8092, PR China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001475

Reference40 articles.

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