Planar Laser-Induced Iodine Fluorescence Measurements in Rarefied Hypersonic Flow
Author(s) -
Eric Cecil
Publication year - 2005
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.1941716
Subject(s) - freestream , mach number , hypersonic speed , planar laser induced fluorescence , boundary layer , jet (fluid) , materials science , shock wave , mechanics , planar , oblique shock , shock (circulatory) , optics , nozzle , physics , laser , laser induced fluorescence , thermodynamics , reynolds number , medicine , computer graphics (images) , computer science , turbulence
A planar laser‐induced fluorescence (PLIF) technique is discussed and applied to measurement of time‐averaged values of velocity and temperature in an I2‐seeded N2 hypersonic free jet facility. Using this technique, a low temperature, non‐reacting, hypersonic flow over a simplified model of a reaction control system (RCS) was investigated. Data are presented of rarefied Mach 12 flow over a sharp leading edge flat plate at zero incidence, both with and without an interacting jet issuing from a nozzle built into the plate. The velocity profile in the boundary layer on the plate was resolved. The slip velocity along the plate, extrapolated from the velocity profile data, varied from nearly 100% down to 10% of the freestream value. These measurements are compared with results of a DSMC solution. The velocity variation along the centerline of a jet issuing from the plate was measured and found to match closely with the correlation of Ashkenas and Sherman. The velocity variation in the oblique shock terminating...
Accelerating Research
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom
Address
John Eccles HouseRobert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom