Effect of swirl on the potential core in two-dimensional ejector nozzles

Author:

Chu Chong-Wei1,Der Joe1,Ortiz Vincent M.1,Widynski Thomas C.1

Affiliation:

1. Northrop Corporation, Hawthorne, California

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. The influence of the adverse pressure gradient on the flow characteristics of a serpentine nozzle with film cooling;Aerospace Science and Technology;2023-05

2. PIV Measurements of Internal Flows through Nozzles with Curvature and Shape Transition;AIAA SCITECH 2023 Forum;2023-01-19

3. A review of jet mixing enhancement for aircraft propulsion applications;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2006-02-01

4. Circular-to-rectangular transition duct flow without and with inlet swirl;Journal of Propulsion and Power;1994-01

5. A unique approach to solve thermal mixing heat transfer problems;25th Joint Propulsion Conference;1989-07-12

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