Study on the Impact of Missile Flight Mach to its Engine Thrust

Rui Qing Liu; Yi Jiang

doi:10.4028/www.scientific.net/AMR.1030-1032.1331

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 1030-1032Study on the Impact of Missile Flight Mach to its...

Study on the Impact of Missile Flight Mach to its Engine Thrust

Abstract:

Rocket engine thrust is the main performance parameters. The flow field of missile fight in different Mach is simulated by using FLUENT, then calculating the thrust of different conditions. The calculating results are consistent with the theory of Mach almost no effect on the thrust.

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Periodical:

Advanced Materials Research (Volumes 1030-1032)

Pages:

1331-1336

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1030-1032.1331

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Online since:

September 2014

Authors:

Rui Qing Liu*, Yi Jiang

Keywords:

Mach, Numerical Simulation, Thrust

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* - Corresponding Author

References

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[4] JIANG Yi, HAO Ji-guang and FU De-bin, in: 3D Unsteady Numerical Simulation of Missile Launching, recorded in Introducing Journal of China Ordnance (2008).

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