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Title: Study of asymmetric supersonic jet flow for ejectors

Conference ·
OSTI ID:6601190
 [1];  [2]; ;  [3];  [4]; ;  [5]
  1. University of Southern California, Los Angeles, CA (USA). Dept. of Aerospace Engineering
  2. BDM, Inc., Seattle, WA (USA)
  3. Flow Research, Inc., Kent, WA (USA)
  4. Boeing Co., Seattle, WA (USA)
  5. Oak Ridge National Lab., TN (USA)

An asymmetric subsonic jet nozzle with a small aspect ratio can entrain a mass several times higher than a circular jet can entrain in a low subsonic flow. In this study, we extend the Mach number of the jet to 2.5. The advantage an asymmetric jet has over a circular jet in enhancing mass transfer still exists in the supersonic range. The main objective of this study is to explore the possibility of applying the asymmetric jet to a supersonic ejector with pressure build-up. The wall confinement was found to have a strong effect on the entrainment.

Research Organization:
Oak Ridge National Lab. (ORNL), Oak Ridge, TN (United States)
Sponsoring Organization:
DOE/CE
DOE Contract Number:
AC05-84OR21400
OSTI ID:
6601190
Report Number(s):
CONF-901109-14; ON: DE90015598
Resource Relation:
Conference: International symposium on gas-liquid two-phase flows in conjunction with the winter annual meeting of the American Society of Mechanical Engineers, Dallas, TX (USA), 25-30 Nov 1990
Country of Publication:
United States
Language:
English