Numerical Simulation of the Aerodynamics of a Scaled Free Jet Altitude Test Facility Model

Author:

Song Dahe1ORCID,Yang Qingzhen2,Fan Jiazheng3ORCID,Du Xubo4,Chen Pengfei5

Affiliation:

1. Ph.D. Candidate, School of Power and Energy, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, China (corresponding author). ORCID: .

2. Professor, School of Power and Energy, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, China.

3. Ph.D. Candidate, Dept. of Mechanical Engineering, City Univ. of Hong Kong, Hong Kong 999077, China. ORCID: .

4. Ph.D. Candidate, School of Power and Energy, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, China.

5. Researcher, AECC Sichuan Gas Turbine Establishment, Hangkong Rd., Mianyang, Sichuan 621000, China; Ph.D. Candidate, School of Power and Energy, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, China; Researcher, Civil Aviation Power Altitude Simulation Key Laboratory of Sichuan Province, Hangkong Rd., Sichuan 621000, China.

Publisher

American Society of Civil Engineers (ASCE)

Reference21 articles.

1. Beale D. K. 2000. “Suppression of secondary vortical flows in nozzles for free-jet ground test facilities.” In Proc. 38th Aerospace Sciences Meeting and Exhibit. Reston VA: American Institute of Aeronautics and Astronautics.

2. Research progress of free jet nozzle technology;Chen P.;Aeroengine,2022

3. Design and simulation of variable area jet nozzle with asymmetrical attitude simulation;Chen P.;J. Mech. Eng. Sci.,2018

4. Cheng T. 2021. “Research on design technology of jet test cell based on forebody simulator.” M.S. thesis Dept. of Power Engineering Nanjing Univ. of Aeronautics and Astronautics.

5. Dhar S. 2006. “Development and validation of small-scale model to predict large wind turbine behavior.” Ph.D. thesis Dept. of Mechanical Engineering Indian Institute of Technology.

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