Experimental Study of Far-Field Radiated Noise Characteristics for the Leading-Edge Slat of a 30P30N Airfoil

Author:

Geng Xin1ORCID,Liu Peiqing2,Guo Hao3ORCID,Hu Tianxiang4,Li Ling5,Liu Yuan6

Affiliation:

1. Ph.D. Student, Key Laboratory of Aero-Acoustics, Ministry of Industry and Information Technology, Beihang Univ., Beijing 100191, China; Ph.D. Student, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China. ORCID: .

2. Professor, Key Laboratory of Aero-Acoustics, Ministry of Industry and Information Technology, Beihang Univ., Beijing 100191, China; Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China.

3. Associate Professor, Key Laboratory of Aero-Acoustics, Ministry of Industry and Information Technology, Beihang Univ., Beijing 100191, China; Associate Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China (corresponding author). ORCID: .

4. Assistant Professor, Key Laboratory of Aero-Acoustics, Ministry of Industry and Information Technology, Beihang Univ., Beijing 100191, China; Associate Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China.

5. Associate Professor, Key Laboratory of Aero-Acoustics, Ministry of Industry and Information Technology, Beihang Univ., Beijing 100191, China; Associate Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China.

6. Ph.D. Student, Key Laboratory of Aero-Acoustics, Ministry of Industry and Information Technology, Beihang Univ., Beijing 100191, China; Ph.D. Student, 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

Reference42 articles.

1. Slat Noise from an MD30P30N Airfoil at Extreme Angles of Attack

2. Aircraft noise reduction technologies: A bibliographic review

3. Choudhari, M., D. P. Lockard, M. G. Macaraeg, B. A. Singer, C. L. Streett, G. R. Neubert, R. W. Stoker, J. R. Underbrink, M. E. Berkman, and M. R. Khorrami. 2002. Aeroacoustic experiments in the Langley low-turbulence pressure tunnel. Washington, DC: National Aeronautics and Space Administration.

4. Effect of Three-Dimensional Shear-Layer Structures on Slat Cove Unsteadiness

5. Numerical investigation of the flow dynamics past a three-element aerofoil

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