22nd Congress of International Council of the Aeronautical Sciences, Harrogate, UK, 28 August - 1st September, 2000
Paper ICAS 2000-3.5.3
EXPERIMENTAL STUDY ON SELF INDUCED EXCITATION PHENOMENA OF OPPOSING JET IN SUPERSONIC FLOW
K. Karashima (1), S.Aso, G. Takami (2), K.Sato (3)
(1) Nishinippon Institute of Technology, Japan;
(2) Kyushu University, Japan;
(3) ISAS, Japan
Keywords: supersonic flows, opposing jets, shock waves
The self-induced oscillations in supersonic
opposing jet to supersonic free stream have
been investigated. In opposing jet flows in
supersonic flows the flow fields have stable
region and unstable region, depending on the
ratio of total pressure of free stream to total
pressure of opposing jet. In the present study
the ratio of total pressure of free stream to total
pressure of opposing jet , P0j/P0, are selected as
0.469, 0.655, 0.984 and 1.51 . Free stream
Mach number and opposing jet Mach number
are 2.5 and 1.5 respectively. The experimental
model consists of semi-spherical nose and
cylindrical body. The flow fields are visualized
by the Schlieren technique and recorded by
high speed video camera. Also pressure
fluctuations on the model surface are measured.
The results show that there are two features in
self-induced shock wave oscillations and bow
shock wave oscillation is observed in lower total
pressure ratio and recompression shock wave
oscillation is observed in higher total pressure
ratio. Also the peak frequencies for both cases
are different. The pressure time history and
instantaneous flow pattern show good
correlations. The global properties of selfindeuced
shock wave oscillation of opposing
jets in supersonic flows have been revealed.
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