Two new techniques for measuring spatially resolved features in high speed air flows are presented. Rayleigh scattering with ultraviolet light yields intensities which are high enough give instantaneous cross sectional images of atmospheric density air with a relatively low energy laser. These images freeze turbulent features and shock structure. They can be used observe shock wave/ boundary layer interactions and to construct spatial correlations which show the average size and shape of these turbulent features as well as the correlated motion of shock structure. Using the RELIEF method, we are able to instantaneously write lines or shaped volume elements into the flow and interrogate them at a later time. This enables us to record instantaneous velocity profiles, each of which gives a frozen image of the turbulent motion of the flow. From numerous such images the average velocity, turbulence intensity and cross stream velocity correlation can be found.

1.
M.
Zimmermann
and
R.B.
Miles
, “Spatially Resolved Flow Visualization of a Wake Using Laser-Induced Fluorescence,” in
Flow Visualization III
, Ed.
W.J.
Yang
, (
Springer-Verlag
,
Berlin
,
1985
), p.
460
.
2.
J.C.
McDaniel
,
B.
Hiller
, and
R.K.
Hanson
, “
Simultaneous Multiple-Point Velocity Measurements Using Laser-Induced Iodine Fluorescence
,”
Optics Letters
8
, No.
1
, (January
1983
), p.
51
.
3.
P.H.
Paul
,
M.P.
Lee
, and
R.K.
Hanson
, “
Molecular Velocity Imaging of Supersonic Flows Using Pulsed Planar Laser-Induced Fluorescence of NO
,”
Optics Letters
14
, No.
9
, (May 1,
1989
), p.
417
.
4.
R.B.
Miles
,
E.
Udd
, and
M.
Zimmermann
, “
Quantitative Flow Visualization in Sodium Vapor Seeded Hypersonic Helium
,”
Applied Physics Letters
32
, (March
1978
), p.
317
.
5.
S.
Cheng
,
M.
Zimmermann
, and
R.B.
Miles
, “
Supersonic Nitrogen Flow Field Measurements with the Resonant Doppler Velocimeter
,”
Applied Physics Letters
43
, No.
2
, (July 15,
1983
), p.
143
.
6.
M.
Smith
,
A.
Smits
, and
R.
Miles
, “
Compressible Boundary Layer Density Cross Sections by UV Rayleigh Scattering
,” (to be published in
Optics Letters
).
7.
R.B.
Miles
,
J.
Connors
,
E.
Markovitz
,
P.
Howard
, and
G.
Roth
, “
Instantaneous Supersonic Velocity Profiles in an Underexpanded Sonic Air Jet by Oxygen Flow Tagging
,”
Phys. Fluids A1
, No.
2
(February
1989
), p.
389
.
8.
M.C.
Escoda
and
M.B.
Long
, “
Rayleigh Scattering Measurements of the Gas Concentration Field in Turbulent Jets
,”
AIAA Journal
21
, (
1983
), p.
81
.
9.
J.M.
Dyer
, “
Rayleigh Scattering Measurements of Time-Resolved Concentrations in a Turbulent Jet
,”
AIAA Journal
17
, (
1979
), p.
972
.
This content is only available via PDF.
You do not currently have access to this content.