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Fig. 17 Variation of anomaly measure calculated by ASSP with
/
Φ
LBO for different port
Ф
positions (L fuel ) permitted by set up with air
fl
ow Q air : a 70 LPM, b 80 LPM, and c 85 LPM
earlier trends of lower
flow rates plotted in Figs. 16 and 17 (Mukhopadhyay et al.
2013 ), which proves that the STSA-detecting LBO technique consistently works
satisfactorily over a wide range of
fl
fl
ow rates.
4 Conclusions
We present an experimental study on a swirl-stabilized, LPG
-
air, and methane
-
air-
fueled dump plane combustor. Experiments carried out at different
fl
ow rates
varying from 70 to 200 lpm with varied degree of fuel
air premixing. Equivalence
ratios are also varied from stoichiometric to LBO limit. Studies have been carried
-
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