Laser vibrometry for combustion diagnostics in thermoacoustic research
暂无分享,去创建一个
[1] Fabrice Giuliani,et al. Mapping the Density Fluctuations in a Pulsed Air-Methane Flame Using Laser-Vibrometry , 2009 .
[2] Erik V. Jansson,et al. Laser vibrometry measurements of vibration and sound fields of a bowed violin , 2006 .
[3] Jakob Woisetschläger,et al. Frequency resolved interferometric detection of local density fluctuations in flames , 2014 .
[4] Stefan Lindner,et al. Interferometrische Messung und Visualisierung von Schallwellen und Turbulenzen (Interferometric Measurement and Visualisation of Acoustic Waves and Vortexes) , 2002 .
[5] W. Sanz,et al. Laser-optical investigation of turbine wake flow , 2003 .
[6] T. Neger,et al. High-accuracy differential interferometry for the investigation of phase objects , 1993 .
[7] Fabrizio Fontaneto,et al. Frequency-resolved interferometric measurement of local density fluctuations for turbulent combustion analysis , 2010 .
[8] Enrico Primo Tomasini,et al. Subsonic jet pressure fluctuation characterization by tomographic laser interferometry , 2013 .
[9] Martin Lauer,et al. Determination of the Heat Release Distribution in Turbulent Flames by Chemiluminescence Imaging , 2011 .
[10] M N.,et al. Experimental investigation of turbine wake flow by interferometrically triggered LDV-measurements , 2000 .
[11] Fabrice Giuliani,et al. Mapping the Density Fluctuations in a Pulsed Air-Methane Flame Using Laser-Vibrometry , 2009 .
[12] Hadi Widjaya. Tjioe. Feedback control of combustion oscillations , 2010 .
[13] W. Marsden. I and J , 2012 .
[14] Ann P. Dowling,et al. FEEDBACK CONTROL OF COMBUSTION OSCILLATIONS , 2005 .
[15] Jakob Woisetschläger,et al. Frequency- and space-resolved measurement of local density fluctuations in air by laser vibrometry , 2006 .
[16] Thierry Schuller,et al. Interferometric determination of heat release rate in a pulsated flame , 2013 .
[17] F. Mohr,et al. Heterodyn-Interferometer zur Vibrationsanalyse / Heterodyne interferometers for vibration analysis , 1990 .