Modification of Eigenmodes in a Cold-Flow Rocket Combustion Chamber by Acoustic Resonators-Reference-Cited by-同舟云学术

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Modification of Eigenmodes in a Cold-Flow Rocket Combustion Chamber by Acoustic Resonators

Published:2019-07 Issue:4 Volume:35 Page:765-779
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Chemnitz Alexander¹,Kings Nancy¹,Sattelmayer Thomas¹

Affiliation:

1. Technical University of Munich, 85748 Garching, Germany

Funder

Deutsche Forschungsgemeinschaft

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Reference20 articles.

1. SuttonG. P.BiblarzO., Rocket Propulsion Elements, 7th ed., Wiley, New York, 2001, p. 352.

2. Resonance Frequencies and Damping of a Combustor Acoustically Coupled to an Absorber

3. Acoustics of Rocket Combustors Equipped with Absorber Rings

4. On the acoustics of rocket combustors equipped with quarter wave absorbers

5. Impact of Absorber Ring Position and Cavity Length on Acoustic Damping

Cited by 1 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. Collaborative Research for Future Space Transportation Systems;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2020-10-27

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