Nacelle Inlet Optimization at High Angles of Attack Based on the Ensemble Indicator Method-Reference-Cited by-同舟云学术

Nacelle Inlet Optimization at High Angles of Attack Based on the Ensemble Indicator Method

Published:2022-03 Issue:2 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Cao Chen¹,Wang Shuyue²^ORCID,Wang Cong³,Zhang Xintao⁴,Sun Gang⁵^ORCID

Affiliation:

1. Ph.D. Candidate, Dept. of Aeronautics & Astronautics, Fudan Univ., 2617 Guanghua Tower(E), 220 Handan Rd., Shanghai 200433, China.

2. Postdoctor, Dept. of Aeronautics & Astronautics, Fudan Univ., 2501 Guanghua Tower(E), 220 Handan Rd., Shanghai 200433, China. ORCID: .

3. Ph.D. Candidate, Dept. of Aeronautics & Astronautics, Fudan Univ., 2501 Guanghua Tower(E), 220 Handan Rd., Shanghai 200433, China.

4. Engineer, AECC Commercial Aircraft Engine Co., Ltd., 3998 Lianhua Rd. (S), Shanghai 200241, China.

5. Professor, Dept. of Aeronautics & Astronautics, Fudan Univ., 2501 Guanghua Tower(E), 220 Handan Rd., Shanghai 200433, China (corresponding author). ORCID: .

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.1943-5525.0001398

Reference28 articles.

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2. Burley R. 1979. “Effect of lip and centerbody geometry on aerodynamic performance of inlets for tilting-nacelle VTOL aircraft.” In Proc. 17th Aerospace Sciences Meeting. Reston VA: American Institute of Aeronautics and Astronautics.

3. Chen J. Y. Wu Z. Wang and A. Wang. 2015. “Nacelle aerodynamic optimization and inlet compatibility.” In Proc. ASME Turbo Expo 2015: Turbine Technical Conf. and Exposition. New York: ASME.

4. Chou D. C. and D. Hwang. 1984. “Boundary layer transition effects on flow separation around V/STOL engine inlets at high incidence.” In Proc. 22nd Aerospace Sciences Meeting. Reston VA: American Institute of Aeronautics and Astronautics.

5. Prediction of Boundary-Layer Flow Separation in V/STOL Engine Inlets

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