A Circuit-Based Dynamic Characteristic Analysis on the Propelling Flow System in Liquid Rockets

Ming Yang; Zhi Chun Yang

doi:10.4028/www.scientific.net/AMR.765-767.227

Paper Titles

Mechanical Ball Milling and Liquid Phase Sintering of Steel-Bonded Cemented Carbide Machining Crumbs
p.210

Application of LED in Marine Fishery
p.213

Study on Principle of Spacecraft Surface Charge and Discharge
p.217

The Research of Permanent Magnet Sealing Technology in Vertical Hot Galvanized Pot
p.222

A Circuit-Based Dynamic Characteristic Analysis on the Propelling Flow System in Liquid Rockets
p.227

Research on the Design Method of Single Rotor Eddy Current Retarder
p.234

Design of Semi Physical Simulation Platform for Autonomous Underwater Vehicle
p.238

A Novel Method of Smooth Fitting for a Class of the Spatial Convex Cavities in the Multiply Connected Domain
p.244

Submarine Maximum Speed's Influence on the Effect of Evading an Incoming Torpedo
p.248

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 765-767A Circuit-Based Dynamic Characteristic Analysis on...

A Circuit-Based Dynamic Characteristic Analysis on the Propelling Flow System in Liquid Rockets

Abstract:

To penetrate into the study of POGO vibration, by taking the LRC equivalent circuit analyzing method, based on two boundary conditions in document [, taking the flow pulse drive into consideration, this paper proposes four boundary conditions specific to the propelling flow system in liquid rockets, and at the same time, complements the mathematic model. Further, by way of network function, under the liquid system flow parameter, this paper infers transfer function expressions, and makes the accurate solution of the natural frequency under every boundary condition. At last, from the statistic point of view, by the method of correlation coefficient, this paper studies the influence that the flow parameter may have on the system natural frequency, and set the major influential liquid flow parameter to the system natural frequency of liquid propelling flow system in liquid rockets.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 765-767)

Pages:

227-233

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.765-767.227

Citation:

Cite this paper

Online since:

September 2013

Authors:

Ming Yang, Zhi Chun Yang

Keywords:

Flow System, Liquid Rockets, Natural Frequency, Network Function, POGO

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] HUNG Huaide, etc. The Vibration Engineering(Second)[M]. Bei Jing: China Astronautics Publishing Hourse, (1995).

Google Scholar

[2] Fenwick. POGO[R]. Rocketdyne's engineering journal of power technology, Spring, 1992. WANG Qizheng. Configuration Coupling Dynamics[M]. Bei Jing: China Astronautics Publishing Hourse, (1999).

Google Scholar

[3] B.W. Oppenheim, S. Rubin. Advanced pogo stability analysis for liquid rockets[J]. Journal of Spacecraft and Rockets, 1992, 30(3).

DOI: 10.2514/3.25524

Google Scholar

[4] S. Rubin. Prevention of coupled structure-propulsion instability(POGO)[J]. NASA Space Vehicle Design Criteria(Structures), SP-8055, (1970).

Google Scholar

[5] S. Rubin. Longitudinal instability of liquid rockets due to propulsion feedback(POGO)[J]. Journal of Spacecraft,V. 3(5): 1188-1195.

DOI: 10.2514/3.28626

Google Scholar

[6] YANG Ming. The Calculation of the intrinsic frequency of the liquid rocket propulsion system[J]. Structure & Environment Engineering, 2009, 36(5): 1-6.

Google Scholar

[7] SUN Bing, WEI Xin, CHI Yuan-cheng, etc. Study on general calculation of natural frequency for liquid engine flow system in launch vehicle[J]. Missile And Space Vehcile, 2009(1): 38-40.

Google Scholar