Numerical Study on the Effect of Vortex Generators on S-Shaped Intake in Propeller Slipstream-Reference-Cited by-同舟云学术

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Numerical Study on the Effect of Vortex Generators on S-Shaped Intake in Propeller Slipstream

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:

Ren Shuili¹^ORCID,Liu Peiqing²

Affiliation:

1. Ph.D. Candidate, Institute of Fluid Mechanics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China. ORCID: .

2. Professor, Institute of Fluid Mechanics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China (corresponding author).

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.1943-5525.0001402

Reference21 articles.

1. Study on computing separating flows within a diffusion inlet S-duct

2. Turboprop engine propulsion for the 1990's

3. Delot A.-L. E. Garnier and D. Pagan. 2011. “Flow control in a high-offset subsonic air intake.” In Proc. 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. & Exhibit. Reston VA: American Institute of Aeronautics and Astronautics.

4. Simulation of Secondary and Separated Flow in Diffusing S Ducts

5. Gea L.-M. 2013. “CFD simulation for S-duct test case using overset grids.” In Proc. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. Reston VA: American Institute of Aeronautics and Astronautics.

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