Flow visualization of compressible vortex structures using density gradient techniques

Mathematical results are derived for the schlieren and shadowgraph contrast variation due to the refraction of light rays passing through two-dimensional compressible vortices with viscous cores. Both standard and small-disturbance solutions are obtained. It is shown that schlieren and shadowgraph produce substantially different contrast profiles. Further, the shadowgraph contrast variation is shown to be very sensitive to the vortex velocity profile and is also dependent on the location of the peak peripheral velocity (viscous core radius). The computed results are compared to actual contrast measurements made for rotor tip vortices using the shadowgraph flow visualization technique. The work helps to clarify the relationships between the observed contrast and the structure of vortical structures in density gradient based flow visualization experiments.

[1]  J. G. Leishman,et al.  Experimental study of rotor wake/body interactions in hover , 1992 .

[2]  J. G. Leishman,et al.  A study of rotor wake development and wake/body interactions in hover , 1991 .

[3]  J. S. Light,et al.  Tip vortex geometry of a hovering helicopter rotor in ground effect , 1993 .

[4]  W. F. Hilton,et al.  The Photography of Airscrew Sound Waves , 1938 .

[5]  J. Sullivan,et al.  An Experimental Investigation of Vortex Rings and Helicopter Rotor Wakes Using a Laser Doppler Velocimeter , 1973 .

[6]  F. X. Caradonna,et al.  The structure of trailing vortices generated by model rotor blades , 1981 .

[7]  Joseph Stuart,et al.  Tilt Wing Propelloplane Design Requirements , 1957 .

[8]  S. Eskinazi,et al.  Decay of a Viscous Trailing Vortex , 1962 .

[9]  W. Menkirch 2. Density Sensitive Flow Visualization , 1981 .

[10]  Fort F. Felker,et al.  Full-scale tilt-rotor hover performance , 1985 .

[11]  Terence A. Ghee,et al.  A study of the rotor wake of a small-scale rotor model in forward flight using laser light sheet flow visualization with comparisons to analytical models , 1992 .

[12]  N. A. Chigier,et al.  Tip vortices: Velocity distributions , 1971 .

[13]  Young I. Cho,et al.  Wide-field shadowgraph flow visualization of tip vortices generated by a helicopter rotor , 1985 .

[14]  G. Vatistas,et al.  A simpler model for concentrated vortices , 1991 .

[15]  Thomas R. Norman,et al.  Rotor Tip Vortex Geometry Measurements Using the Wide-Field Shadowgraph Technique , 1986 .

[16]  Thomas R. Norman,et al.  Application of the Wide-Field Shadowgraph Technique to Helicopters in Forward Flight , 1992 .

[17]  M. Scully,et al.  Computation of helicopter rotor wake geometry and its influence on rotor harmonic airloads , 1975 .

[18]  Daniel Bershader Quantitative study of the compressible vortex - Generation, structure and interaction with airfoils , 1987 .

[19]  Stephen B. Jones,et al.  A synchronous strobed laser light sheet for rotor flow visualization , 1991 .

[20]  Boeing,et al.  Application of Vortex Visualization Test Techniques to Rotor Noise Research , 1970 .

[21]  J. Gordon Leishman,et al.  Improved wide-field shadowgraph set-up for rotor wake visualization , 1992 .