Refractive-Index-Matching Laser Velocimetry (RIMLV) obtains velocity distributions inflow through complex geometries. Laser velocimetry is used to measure the flow of a constant-temperature mixture that has the refractive index of acrylic models. This mixture can be used to obtain duct Reynolds numbers in the turbulent regime at moderate expense. Measurements can be obtained at desired locations, specifically inside complex models even if laser beams pass through multiple curved surfaces, which is advantageous when comparing measured and calculated results.
Issue Section:
Technical Briefs
1.
Dybbs, A., and Edwards, R. V., 1987, “Refractive Index Matching for Difficult Situations,” 2nd International Conference on Laser Anemometry—Advances and Applications, Paper II, Sept.
2.
Elphick, I. G., Martin, W. W., and Currie, I., G., 1982, “Application of LDA to High Reynolds Number Cross Flow,” Proceedings of the International Symposium on Application of Laser Anemometry to Fluid Mechanics, Superior Technico, Lisbon, Portugal, July, pp. 15.1.1–15.1.12.
3.
Longmire
E. K.
Eaton
J. K.
1992
, “Structure of a Particle-Laden Round Jet
,” Journal of Fluid Mechanics
, Vol. 236
, pp. 217
–257
.4.
Liu
C. H.
Vafidis
C.
Whitelaw
J. H.
1994
, “Flow Characteristics of a Centrifugal Pump
,” ASME JOURNAL OF FLUIDS ENGINEERING
, Vol. 116
, June, pp. 303
–309
.5.
Nouri
J. M.
Whitelaw
J. H.
Yianneskis
M.
1986
, “Particle Motion and Turbulence in Dense Two-Phase Flows
,” International Journal of Multiphase Flow
, Vol. 13
, No. 6, pp. 729
–739
.6.
Park
J. T.
Mannheimer
R. J.
Grimley
T. A.
Morrow
T. B.
1989
, “Pipe Flow Measurements of a Transparent Non-Newtonian Slurry
,” ASME JOURNAL OF FLUIDS ENGINEERING
, Vol. III
, Sept., pp. 331
–336
.7.
Tindal, M. J., Cheung, R. S., and Yianneskis, M., 1988, “Velocity Characteristics of Steady Flows Through Engine Inlet Ports and Cylinders,” Society of Automotive Engineers Paper 880383, Warrendale, PA, Feb.
8.
Thompson, B. E., 1990, “Refractive-Index Matching Techniques in Complex Rocket-Engine Flow Configurations,” Scientific Research Associates Report R89-900072-F, Glastonbury, Ct.
9.
Thompson
B. E.
Senaldi
J.
Vafidis
C.
Whitelaw
J. H.
McDonald
H.
1992
, “Flow in a Model of the Space Shuttle Main Engine Main Injector Bowl
,” Journal of Spacecraft and Rockets
, Vol. 29
, Mar.-Apr., pp. 247
–252
.10.
Waesche
R. H. W.
Sargent
W. H.
1989
, “Space Shuttle Solid Rocket Motor Aft-End Internal Flows
,” Journal of Propulsion and Power
, Vol. 5
, Nov.-Dec, pp. 650
–656
.
This content is only available via PDF.
Copyright © 1998
by The American Society of Mechanical Engineers
You do not currently have access to this content.