Jing-feng YE, Jun SHAO, Guo-hua LI, et al. Vibration disturbance suppression in velocity measurements by hydroxyl tagging velocimetry[J]. Optics and precision engineering, 2017, 25(7): 1689-1696.
DOI:
Jing-feng YE, Jun SHAO, Guo-hua LI, et al. Vibration disturbance suppression in velocity measurements by hydroxyl tagging velocimetry[J]. Optics and precision engineering, 2017, 25(7): 1689-1696. DOI: 10.3788/OPE.20172507.1689.
Vibration disturbance suppression in velocity measurements by hydroxyl tagging velocimetry
In order to suppress the strong vibration disturbance in Hydroxyl Tagging Velocimetry(HTV) in practical experimental environment for an engine
the characteristic of radiation spectrum of tagging laser interacted with different flow fields was analyzed experimentally. In the experiment
two strategies for vibration disturbance suppression were designed by capturing the tagging laser image and moved tagging image simultaneously. For a general flow field
the Rayleigh scattering of the tagging laser was used as reference images
and in a combustion flow field which contained unburned large hydrocarbon fuel like kerosene
CH
4
the radiation of the tagging laser induced fuel in the waveband of OH fluorescence spectrum was taken as reference images. The velocity measurement in the flow field of a scramjet engine indicates that the two approaches can suppress the vibration disturbance efficiently. Moreover
the Rayleigh scattering image of the tagging laser is disturbed by wall scattering in the relative pure flow region
making the uncertainty of the base tagging position identification approximate to 0.06 mm. In the follow region with abundant unburned fuels
the latter method can obtain comparatively clear tagging laser images with the uncertainty of base tagging position identification reduced to 0.03 mm
which equals to the uncertainty of the average method.
关键词
Keywords
references
KOOCHESFAHANI M. Molecular tagging velocimetry (MTV)-progress and applications[C]. 30th Fluid Dynamics Conference, AIAA, 1999-3786.
DEBARBER PA, SEGALL J, BROWN M S, et al.. Ozone flow tagging-a novel approach for unseeded velocity measurement[C]. 26th Plasmadynamics and Lasers Conference, AIAA, 1995-1952.
MICHAEL J B, EDWARDS M R, DOGARIU A, et al.. Femtosecond laser electronic excitation tagging for quantitative velocity imaging in air[J]. Applied Optics, 2011, 50(26):5158-5162.
DAM N, KLEIN-DOUWEL R J H, SIJTSEMA N M, et al.. Nitric oxide flow tagging in unseeded air[J]. Optics Letters, 2001, 26(1):36-38.
SHI X CH, WANG J, XIAO X H, et al.. Tagging procedures of Raman excitation plus laser induced electronic fluorescence flow velocimetry[J]. Acta Optica Sinica, 2001, 21(2):206-210. (in Chinese)
WANG P Y, XING F. Advanced laser measurement technology for aeroengine combustor research and development[J]. Aeroengine, 2012, 38(4):53-58. (in Chinese)
ISMAILOVM M, SCHOCK H J, FEDEWA A M. Gaseous flow measurements in an internal combustion engine assembly using molecular tagging velocimetry[J]. Experiments in Fluids, 2006, 41(1):57-65.
DANEHY P M, O'BYRNE S, HOUWING A F P, et al.. Flow-tagging velocimetry for hypersonic flows using fluorescence of nitric oxide[J]. AIAA Journal, 2003, 41(2):263-271.
MICHAEL J B, EDWARDS M R, DOGARIU A, et al.. Femtosecond laser electronic excitation tagging for quantitative velocity imaging in air[J]. Applied Optics, 2011, 50(26):5158-5162.
MIRZAEI M, DAM N J, VAN DE WATER W. Molecular tagging velocimetry in turbulence using biacetyl[J]. Physical Review E, 2012, 86(4):046318.
SHIRLEYJ A, BOEDEKER L R. Non-intrusive space shuttle main engine nozzle exit diagnostics[C]. 24th Joint Propulsion Conference, AIAA, 1988-3088.
WEHRMEYER J A, RIBAROV L A, OGUSS D A, et al.. Flame flow tagging velocimetry with 193-nm H 2 O photodissociation[J]. Applied Optics, 1999, 38(33):6912-6917.
PITZ R, LAHR M D, DOUGLAS Z W, et al.. Hydroxyl tagging velocimetry in a supersonic flow over a cavity[J]. Applied Optics, 2005, 44(31):6692-6700.
PERKINS A N, RAMSEY M, PITZ R W, et al.. Investigation of a bow shock in a shock tube flow facility using hydroxyl tagging velocimetry (HTV)[C]. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Aerospace Sciences Meetings, AIAA, 2011-1092.
YE J F, SHAO J, LI G H, et al.. Supersonic flow velocity measurements by hydroxyl tagging velocimetry[C]. The Proceedings of the 16 th National Symposium on Shock Wave, 2014:363-368. (in Chinese)
ALEXANDER A, WEHRMEYER J, RUNGE W, et al.. Nonintrusive measurement of gas turbine exhaust velocity using hydroxyl tagging velocimetry[C]. 26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Fluid Dynamics and Co-located Conferences, AIAA, 2008-235.
BLANFORD B T, RUNGE W O, HU S T, et al.. Application of hydroxyl tagging velocimetry (HTV) to measure centerline velocities in the near field exhaust of a gas turbine engine[C]. 46th AIAA Aerospace Sciences Meeting and Exhibit, AIAA, 2008-235.
INMAN J A, DANEHY P M, BATHEL B, et al. Laser-induced fluorescence velocity measurements in supersonic underexpanded impinging jets[C]. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA, 2010-1438.
PERKINS A N, RAMSEY M, STRICKLAND D J, et al.. Dual-pulse hydroxyl tagging velocimetry (HTV) in jet engine exhausts[C]. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Joint Propulsion Conferences, AIAA, 2009-5108.
RAMSEY M C, PITZ R W. Template matching for improved accuracy in molecular tagging velocimetry[J]. Experiments in Fluids, 2011, 51(3):811-819.
Velocity measurements in supersonic mixing layer using femtosecond laser electronic excitation tagging
Two-dimensional point laser Doppler velocimeter for velocity measurement
Measurement of impact points using reflective light screen target of single column light source
Related Author
CHEN Li
YIN Yimin
LI Yudong
LI Meng
CHEN Shuang
LI Xiu-ming
HUANG Zhan-hua
LI Xiang-yu
Related Institution
Facility Design and Instrumentation Institute, China Aerodynamics Research and Development Center
State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center
Key Laboratory of Opto-electronics Information Technology of the Ministry of Education, College of Precision Instrument and Optoelectronics Engineering, Tianjin University