Numerical Study on Mechanism of Drag Reduction by Microblowing Technique on Supercritical Airfoil-Reference-Cited by-同舟云学术

Numerical Study on Mechanism of Drag Reduction by Microblowing Technique on Supercritical Airfoil

Published:2017-05 Issue:3 Volume:30 Page:04016084
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Gao Zhenxun¹,Cai Junxuan²,Li Jian³,Jiang Chongwen⁴,Lee Chun-Hian⁵

Affiliation:

1. Assistant Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China (corresponding author).

2. Graduate Student, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China.

3. Engineer, Beijing Aerospace Technology Institute, Beijing 100074, China.

4. Assistant Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China.

5. Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000685

Reference25 articles.

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2. Cook P. H. Mcdonald M. A. and Firmin M. C. P. (1979). “Aerofoil RAE2822—Pressure distributions and boundary layer and wake measurements. Experimental data base for computer program assessment.” AGARD Rep. No. AR 138 North Atlantic Treaty Organization Neuilly sur Seine France.

3. Feiz H. and Menon S. (2003). “LES of multiple jets in crossflow using a coupled lattice Boltzmann-finite volume solver.” Proc. 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit American Institute of Aeronautics and Astronautics Reston VA.

4. Improvement and application of wall function boundary condition for high-speed compressible flows

5. A new wall function boundary condition including heat release effect for supersonic combustion flows

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