Mixer-Ejector Noise-Suppressor Model-Reference-Cited by-同舟云学术

Mixer-Ejector Noise-Suppressor Model

Published:1998-11 Issue:6 Volume:14 Page:941-950
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Tew David E.¹,Teeple Brian S.¹,Waitz Ian A.¹

Affiliation:

1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

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/10.2514/2.5358

Reference11 articles.

1. Enhanced mixing with streamwise vorticity

2. 2Elliott, J. K. "A Computational Investigation of the Fluid Dynamics of a Three-Dimensional Compressible Mixing Layer with Strong Streamwise Vorticity," M.S. Thesis, Massachusetts Inst. of Technology, Cambridge,MA, 1990.

3. 3Qiu, Y. J. "A Study of Streamwise Vorticity Enhanced Mixing in Lobed Mixer Devices," Ph.D. Dissertation, Massachusetts Inst. of Technology, Cambridge,MA, 1992.

4. 4Manning, T. A. "Experimental Studies of Mixing Flows with Streamwise Vorticity," M.S. Thesis, Massachusetts Inst. of Technology, Cambridge,MA, 1991.

Cited by 13 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. Effect of Number and Spacing of Pre-cooled Turbojet Engines on Takeoff Noise of Hypersonic Transport;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2024

2. Acoustic Characteristics of Rectangular Hypersonic Mixer Ejector;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023

3. Variable Mixing Nozzle Design with Slotted Vortex Generators for Jet Noise Reduction;AIAA AVIATION 2020 FORUM;2020-06-08

4. Mechanisms of lobed jet mixing: About circularly alternating-lobe mixers;Aerospace Science and Technology;2020-03

5. Effects of shear layer growth on the indirect noise in compound nozzles;Journal of Sound and Vibration;2020-03