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Nozzle Damping of the Fluidic Nozzle

Name: Nozzle Damping of the Fluidic Nozzle
Keywords: 7. Clean energy

descriptionPublicationkeyboard_double_arrow_right Part of book or chapter of book , Other literature type 01 Jan 2019 English Publisher:Springer Singapore

Authors: Junwei Li; Yu Liu; Xinmin Chen; Kan Xie;

doi: 10.1007/978-981-13-6439-6_9

Nozzle Damping of the Fluidic Nozzle

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Abstract

For a thrust-adjustable rocket motor, to avoid unstable combustion, we not only need to consider nozzle damping before thrust adjustment, but also need to consider nozzle damping variation thereafter, and it is important to learn about the influence of nozzle damping before, and after, thrust adjustment. This chapter discusses wave attenuation method for predicting nozzle damping of the fluidic nozzle, validation of numerical prediction method for nozzle damping, and gives the nozzle damping variation with different secondary flow parameters.

Related Organizations

Beihua University
China (People's Republic of)
China Academy of Launch Vehicle Technology
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Beihang University
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Beijing Institute of Technology
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Impact byBIP!

	citations This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	0
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	influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	Average
	impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.	Average