A Comparison of the Nonlinear Unsteady Responses of Two Classical Models for Solid Propellant-Reference-Cited by-同舟云学术

A Comparison of the Nonlinear Unsteady Responses of Two Classical Models for Solid Propellant

Published:2022-07-20 Issue: Volume: Page:
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Container-title:2022 13th International Conference on Mechanical and Aerospace Engineering (ICMAE)
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Author:

Wang Zhuopu¹,Zhang Xiangyu²,Bai Yanjun²,Gan Xiaosong²,Wang Jianru²,Jin Bingning¹,Liu Peijin¹

Affiliation:

1. Northwestern Polytechnical University,Science and Technology on Combustion, Internal Flow and Thermo-Structure Laboratory,Xi'an,People's Republic of China

2. The Fourth Academy of CASC,The 41st Institute of Fourth Academy of CASC,Xi'an,People's Republic of China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9852822/9852497/09852891.pdf?arnumber=9852891

Reference11 articles.

1. Pulsed instabilities in solid-propellant rockets

2. Aluminum Combustion Can Drive Instabilities in Solid Rocket Motors: T-Burner Study

3. Combustion of Energetic Materials in an Acoustic Field (Review)

4. Thermoacoustic instability in a solid rocket motor: non-normality and nonlinear instabilities

5. Non-linear analysis of solid propellant burning rate behavior

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