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Performance calculations and analysis of multi-module aerospike nozzles with round to rectangle inner nozzles

Research output: Contribution to journalArticlepeer-review

Abstract

Based on an non-oscillatory and non-free parameters dissipation difference (NND) scheme to solve three-dimensional Reynolds averaged Navier-Stokes equations, performance calculations and analysis of multi-module aerospike nozzles with round to rectangle inner nozzles were investigated. Flow characteristics and performance of four inner nozzles including bell nozzle, two-dimensional nozzle, round to square inner nozzle and square throat to square exit nozzle were compared. Then performance of round to rectangle inner nozzles that have different structures such as contour changing points, contours after changing points and exit arc radiuses were discussed. The effects of different structures of inner nozzles, different nozzle obliquities and different plug contours on the multi-module linear aerospike nozzles were also presented. And a design scheme of the optimized aerospike nozzle was given. Conclusions can provide some reference for studying design of the multi-module linear aerospike nozzles with round to rectangle inner nozzles.

Original languageEnglish
Pages (from-to)639-644
Number of pages6
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume22
Issue number4
StatePublished - Apr 2007

Keywords

  • Aerospace propulsion system
  • Aerospike nozzle
  • Performance
  • Plug contour
  • Round to rectangle inner nozzle

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