Surface Roughness Effects on Unsteady Transition Property over a Pitching Airfoil-Reference-Cited by-同舟云学术

Surface Roughness Effects on Unsteady Transition Property over a Pitching Airfoil

Published:2022-05 Issue:3 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Li Yi¹,Xu Jiakuan²,Zhang Yang³,Bai Junqiang⁴

Affiliation:

1. Ph.D. Candidate, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

2. Associate Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China (corresponding author).

3. Associate Professor, State Key Laboratory for Mechanical Structural Strength and Vibration, Xi’an Jiaotong Univ., Xi’an 710049, China.

4. Professor, Unmanned System Research Institute, Northwestern Polytechnical Univ., Xi’an 710072, 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.1943-5525.0001404

Reference28 articles.

1. Transitional boundary layer study over an airfoil in combined pitch-plunge motions

2. A Review of Surface Roughness Effects in Gas Turbines

3. Dassler P. D. Kožulovic and A. Fiala. 2010. “Transport equation for roughness effects on laminar-turbulent transition.” In Proc. 5th European Conf. on Computational Fluid Dynamics. Lisbon Portugal: European Community on Computational Methods in Applied Sciences.

4. Untersuchungen über die abhängigkeit des umschlages laminar-turbulent von der oberflächenrauhigkeit und der druckverteilung;Feindt E. G.;Schiffbautechn,1957

5. Effects of leading edge defects on aerodynamic performance of the S809 airfoil

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