Investigation on Incompressible Lobed Mixer–Ejector Performance-Reference-Cited by-同舟云学术

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Investigation on Incompressible Lobed Mixer–Ejector Performance

Published:2015-01 Issue:1 Volume:31 Page:265-277
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Shan Yong¹,Pan Cheng-xiong¹,Zhang Jing-zhou¹

Affiliation:

1. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35279

Reference40 articles.

1. PreszW. M. “Mixer/Ejector Noise Suppressors,” AIAA Paper 1991-2243, 1991.

2. PreszW. M.ReynoldsG.McCormickD. C. “Thrust Augment Using Mixer-Ejector-Diffuser Systems,” AIAA Paper 1994-0020, 1994.

3. Internal Aerodynamics of Infrared Suppressors for Helicopter Engines

4. PreszW. M.BlinnR. F.MorinB. L. “Short Efficient Ejector Systems,” AIAA Paper 1987-1837, 1987.

5. Forced mixer lobes in ejector designs

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2. Mechanisms of lobed jet mixing: Comparison of bilinear, rectangular, and circular lobed mixers;Aerospace Science and Technology;2023-11

3. Numerical Investigation of Air Entrainment and Outlet Temperature Characteristics of a Convex-Type Infrared Suppression Device;Journal of Heat Transfer;2022-09-29

4. Air Entrainment and Outlet Temperature Characteristics of a Modified Infrared Suppression Device With Inward and Outward Guides;Journal of Thermal Science and Engineering Applications;2022-08-24

5. Configuration of the lobed nozzle in an ejector mixer for extreme mixing efficiency;International Journal of Heat and Mass Transfer;2022-02

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