Hydroxyl tagging velocimetry in a supersonic flow over a cavity.

Hydroxyl tagging velocimetry (HTV) measurements of velocity were made in a Mach 2 (M 2) flow with a wall cavity. In the HTV method, ArF excimer laser (193 nm) beams pass through a humid gas and dissociate H2O into H + OH to form a tagging grid of OH molecules. In this study, a 7 x 7 grid of hydroxyl (OH) molecules is tracked by planar laser-induced fluorescence. The grid motion over a fixed time delay yields about 50 velocity vectors of the two-dimensional flow in the plane of the laser sheets. Velocity precision is limited by the error in finding the crossing location of the OH lines written by the excimer tag laser. With a signal-to-noise ratio of about 10 for the OH lines, the determination of the crossing location is expected to be accurate within +/- 0.1 pixels. Velocity precision within the freestream, where the turbulence is low, is consistent with this error. Instantaneous, single-shot measurements of two-dimensional flow patterns were made in the nonreacting M 2 flow with a wall cavity under low- and high-pressure conditions. The single-shot profiles were analyzed to yield mean and rms velocity profiles in the M 2 nonreacting flow.

[1]  H. Rubinsztein-Dunlop,et al.  Velocity measurements by flow tagging employing laser enhanced ionisation and laser induced fluorescence , 1995 .

[2]  Ronald K. Hanson,et al.  Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview , 2001 .

[3]  R. Hanson,et al.  Simultaneous multiple-point velocity measurements using laser-induced iodine fluorescence. , 1983, Optics letters.

[4]  W. Kessler,et al.  Velocity Field Imaging in Supersonic Reacting Flows near Atmospheric Pressure , 1994 .

[5]  Campbell D. Carter,et al.  Mixing and combustion studies using cavity-based flameholders in a supersonic flow , 2004 .

[6]  G. Gauba,et al.  OH laser-induced fluorescence velocimetry technique for steady, high-speed, reacting flows , 1994 .

[7]  R. Hanson,et al.  Continuous wave laser absorption techniques for gasdynamic measurements in supersonic flows. , 1991, Applied optics.

[8]  N. Jiang,et al.  Molecular Tagging Velocimetry Measurements in Supersonic Microjets , 2002 .

[9]  R. Pitz,et al.  Ozone Tagging Velocimetry Using Narrowband Excimer Lasers , 1999 .

[10]  G. Laufer,et al.  Laser ion time-of-flight velocity measurements using N2(+) tracers , 1995 .

[11]  Joseph A. Wehrmeyer,et al.  Multiline hydroxyl tagging velocimetry measurements in reacting and nonreacting experimental flows , 2004 .

[12]  Paul M. Danehy,et al.  Flow-Tagging Velocimetry for Hypersonic Flows Using Fluorescence of Nitric Oxide , 2001 .

[13]  R. Pitz,et al.  Flame flow tagging velocimetry with 193-nm H2O photodissociation. , 1999, Applied optics.

[14]  M. Koochesfahani,et al.  Molecular Tagging Velocimetry (MTV) measurements in gas phase flows , 1999 .

[15]  L. Boedeker,et al.  Velocity measurement by H2O photolysis and laser-induced fluorescence of OH. , 1989, Optics letters.

[16]  L. Drain The Laser Doppler Technique , 1980 .

[17]  M. Koochesfahani,et al.  The accuracy of remapping irregularly spaced velocity data onto a regular grid and the computation of vorticity , 2000 .

[18]  Richard B. Miles,et al.  Hypersonic‐helium‐flow‐field measurements with the resonant Doppler velocimeter , 1980 .

[19]  Walter R. Lempert,et al.  QUANTITATIVE FLOW VISUALIZATION IN UNSEEDED FLOWS , 1997 .

[20]  P. Danehy,et al.  Laminar boundary layer separation at a fin-body junction in a hypersonic flow , 2001 .

[21]  K. Hsu,et al.  Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors , 1999 .

[22]  C. D. Scott,et al.  Copper atom based measurements of velocity and turbulence in arc jet flows , 1991 .

[23]  J. Daily,et al.  Combustion in a turbulent mixing layer formed at a rearward-facing step , 1983 .

[24]  Campbell D. Carter,et al.  Characteristics of Cavity-Stabilized Flames in a Supersonic Flow , 2005 .

[25]  P. Dimotakis,et al.  Unseeded molecular flow tagging in cold and hot flows using ozone and hydroxyl tagging velocimetry , 2000 .

[26]  J. J. ter Meulen,et al.  Molecular tagging velocimetry in the wake of an object in supersonic flow , 2003 .

[27]  R. Hanson,et al.  Velocity visualization in gas flows using laser-induced phosphorescence of biacetyl , 1984 .

[28]  P. A. Skaggs,et al.  Unseeded velocity measurement by ozone tagging velocimetry. , 1996, Optics letters.

[29]  Richard A. Yetter,et al.  Hydroxyl tagging velocimetry (HTV) in experimental air flows , 2002 .

[30]  N. Dam,et al.  Air photolysis and recombination tracking : A new molecular tagging velocimetry scheme , 2002 .

[31]  Mark Gruber,et al.  New supersonic combustion research facility , 1995 .

[32]  U. Frisch,et al.  Transverse velocity increments in turbulent flow using the RELIEF technique , 1997, Journal of Fluid Mechanics.

[33]  R. Hanson,et al.  Molecular velocity imaging of supersonic flows using pulsed planar laser-induced fluorescence of NO. , 1989, Optics Letters.

[34]  R. Adrian Particle-Imaging Techniques for Experimental Fluid Mechanics , 1991 .

[35]  M. Maurice LASER VELOCIMETRY SEED PARTICLES WITHIN COMPRESSIBLE, VORTICAL FLOWS , 1992 .

[36]  Spectrally resolved Rayleigh scattering diagnostic for hydrogen-oxygen rocket plume studies , 1991 .

[37]  N M Sijtsema,et al.  Nitric oxide flow tagging in unseeded air. , 2001, Optics letters.

[38]  Robert J. Santoro,et al.  Testing at university facilities , 2001 .

[39]  Manoochehr Koochesfahani,et al.  A spatial correlation technique for estimating velocity fields using molecular tagging velocimetry (MTV) , 1996 .

[40]  Jürgen Wolfrum,et al.  NO-FLOW TAGGING BY PHOTODISSOCIATION OF NO2. A NEW APPROACH FOR MEASURING SMALL-SCALE FLOW STRUCTURES , 1999 .