Parametric investigation of controlling factors for deceleration and evacuation qualities by supersonic diffuser

Byung Hoon Park, Ji Hwan Lim, Woongsup Yoon, Ji Hyung Lee, Yeol Lee

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Essential geometric and operating factors controlling steady performance characteristics and starting transients of a straight axi-symmetric supersonic exhaust diffuser with zero-secondary flows are studied experimentally and numerically. Static pressure distributions along the diffuser wall and vacuum chamber pressure records are measured by a small-scale simulator using cold nitrogen gas as a working fluid. Preconditioned Favre-averaged Navier-Stokes equations with turbulence compressibility effects incorporated into low Reynolds number k-E turbulence model are employed to solve steady and unsteady flow-fields in the diffuser. The fact that the mode transition of a small L/D supersonic diffuser occurs at higher nozzle inlet total pressure than the optimum starting pressure of a large L/D supersonic diffuser is visualized numerically. In the mode transition regime, a sudden drop of vacuum chamber pressure during a starting transient observed in the measured data is numerically reproduced and the retardation of the supersonic jet impingement is shown to be the primary cause for the jumping mode transition. Abrupt shrinking of the internal shock structure is observed experimentally as the nozzle inlet total pressure decreases; however, this makes no significant alteration to the vacuum chamber pressure, as long as the nozzle inlet total pressure is greater than the diffuser starting pressure. In addition, the vacuum chamber pressure is promptly equilibrated by the low initial cell pressure, due to the rapid expansion of the under-expanded supersonic jet from the nozzle exit immediately followed by opening the diffuser exit port cover. In this case, due to the strongly reversed nozzle exhaust flow into the vacuum chamber, locally supersonic flow structure emerges momentarily in the vacuum chamber.

Original languageEnglish
Title of host publicationCollection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages957-976
Number of pages20
ISBN (Print)1563478188, 9781563478185
DOIs
Publication statusPublished - 2006 Jan 1
EventAIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference - Sacramento, CA, United States
Duration: 2006 Jul 92006 Jul 12

Publication series

NameCollection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
Volume2

Other

OtherAIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
CountryUnited States
CitySacramento, CA
Period06/7/906/7/12

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Energy(all)
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

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  • Cite this

    Park, B. H., Lim, J. H., Yoon, W., Lee, J. H., & Lee, Y. (2006). Parametric investigation of controlling factors for deceleration and evacuation qualities by supersonic diffuser. In Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference (pp. 957-976). (Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference; Vol. 2). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2006-4415