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Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shifta)
a)This paper was first presented as AIAA Paper 2004-4054 at the 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, Florida, 11–14 July 2004 and was the winner of the 2004 AIAA Solid Rockets Best Paper award.
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10.1063/1.2746042
/content/aip/journal/pof2/19/9/10.1063/1.2746042
http://aip.metastore.ingenta.com/content/aip/journal/pof2/19/9/10.1063/1.2746042
View: Figures

Figures

Image of FIG. 1.
FIG. 1.

Nonlinear instability effects.

Image of FIG. 2.
FIG. 2.

Transition to limit cycle in T-burner [Jensen and Beckstead (Ref. 34)].

Image of FIG. 3.
FIG. 3.

Mean and oscillating pressure [Brownlee (Ref. 15)].

Image of FIG. 4.
FIG. 4.

Measured vs theoretical growth rates [Blomshield (Ref. 37)].

Image of FIG. 5.
FIG. 5.

Culick’s fully steepened wave.

Image of FIG. 6.
FIG. 6.

Nonlinear evolution of system amplitude.

Image of FIG. 7.
FIG. 7.

Measured vs calculated waveform: (a) waveform calculated using twenty modes in Eq. (1) and (b) waveform measured experimentally in a preburner undergoing severe oscillation.

Image of FIG. 8.
FIG. 8.

Shock layer structure.

Image of FIG. 9.
FIG. 9.

Measured (a) and simulated (b) pressure vs time for motor No. 9 [Blomshield (37)].

Image of FIG. 10.
FIG. 10.

Same comparison for Motor No. 10.

Image of FIG. 11.
FIG. 11.

Same comparison for Motor No. 13.

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/content/aip/journal/pof2/19/9/10.1063/1.2746042
2007-09-05
2014-04-23
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752b84549af89a08dbdd7fdb8b9568b5 journal.articlezxybnytfddd
Scitation: Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shifta)
http://aip.metastore.ingenta.com/content/aip/journal/pof2/19/9/10.1063/1.2746042
10.1063/1.2746042
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