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Title: Combustion enhancement of a premixed flame by acoustic forcing with emphasis on role of large-scale vortical structures

Conference ·
OSTI ID:6170151
; ;  [1]
  1. Naval Weapons Center, China Lake, CA (USA) Stanford Univ., CA (USA) Ecole Centrale des Arts et Manufactures, Chatenay-Malabry (France)

The response of a chemically reacting, turbulent shear flow subject to flow excitation is studied in a two-dimensional, laboratory combustor. The combustor employs a V-shaped bluff-body flame holder. A premixed propane-air mixture flows over the flame holder creating two turbulent mixing layers, in which combustion is initiated. The inlet flow is periodically surged by acoustically forcing the upstream flow and the flame response is investigated in the near wake region behind the stabilizer. Experimental observations combine acoustic pressure measurements, C2 radical spectroscopy, and direct-shadow spark visualization. It is shown that forcing may produce significant increases in overall combustion rate by generating periodic large-scale vortical structures. These orderly structures accelerate the entrainment and improve the mixing between incoming fresh reactants and recirculating hot gases. The magnitude of the increase is a sensitive function of forcing frequency. Data indicate that maximum combustion enhancement occurs when the forcing frequency matches the preferred mode of the hydrodynamic field in the near wake region. 13 refs.

OSTI ID:
6170151
Report Number(s):
AIAA-Paper-91-0367; CONF-910117-
Resource Relation:
Conference: 29. AIAA aerospace sciences conference, Reno, NV (USA), 7-10 Jan 1991
Country of Publication:
United States
Language:
English