Abstract
OH planar laser-induced fluorescence (PLIF) and particle image velocimetry (PIV) have been used to study the frequency response of laminar CsHg-air counterflow diffusion flames, and thereby the adequacy of the steady-flamelet model for turbulence. PIV was used to determine the flame strain rate, while OH PLIF was used both to measure temperature at the flame front, using the two- line PLIF technique, and the reaction-zone width. Both measurements demonstrate the existence of a diffusion-limited frequency response of flames subjected to a time-varying flow field. At the 30-Hz and 50-Hz forcing frequencies, the maximum reaction-zone temperature and width were found to respond quasi-steadily. However, At higher forcing frequencies-that is, 100 and 200 Hz-transient behavior is evident from the phase relationship between the imposed sinusoidal strain rate and the resulting peak temperature and reaction-zone width. The measured values of the OH-field widths (FWHM) were fit well by an offset sine function. In all cases when the oscillation amplitude (from the sine-curve fit) is normalized by the cycle mean strain rate and plotted against the non-dimensional flow field frequency, it collapses onto a single line with a steep negative slope.
Original language | English (US) |
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State | Published - 2001 |
Externally published | Yes |
Event | 39th Aerospace Sciences Meeting and Exhibit 2001 - Reno, NV, United States Duration: Jan 8 2001 → Jan 11 2001 |
Other
Other | 39th Aerospace Sciences Meeting and Exhibit 2001 |
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Country/Territory | United States |
City | Reno, NV |
Period | 01/8/01 → 01/11/01 |
ASJC Scopus subject areas
- Space and Planetary Science
- Aerospace Engineering