DocumentCode
2903151
Title
A laser-induced heat flux technique for convective heat transfer measurements in high speed flows
Author
Porro, A.R. ; Keith, T.G., Jr. ; Hingst, W.R.
Author_Institution
NASA Lewis Res. Center, Cleveland, OH, USA
fYear
1991
fDate
27-31 Oct 1991
Firstpage
146
Lastpage
155
Abstract
Infrared thermography was used to monitor surface model temperatures with an applied heat flux due to a laser heating source in a supersonic flowfield. The technique was used to measure the local surface convective heat transfer coefficient distribution on a flat plate at nominal Mach numbers of 2.5, 3.0, 3.5, and 4.0. The flat plate boundary layer initially was laminar and became transitional in the measurement region. The experimentally determined convective heat transfer coefficients were generally higher than the theoretical predictions for flat plate laminar boundary layers. However, the results indicate that this nonintrusive optical measurement technique has the potential to measure surface convective heat transfer coefficients in high-speed flowfields
Keywords
boundary layers; convection; flow measurement; infrared imaging; laminar to turbulent transitions; laser beam applications; supersonic flow; wind tunnels; IR imaging; boundary layer; convective heat transfer coefficients; convective heat transfer measurements; flat plate; heat flux; laminar boundary layers; laser heating source; laser-induced heat flux; nonintrusive optical measurement; supersonic flowfield; surface model temperatures; transitional flow; Heat transfer; High speed optical techniques; Infrared heating; Infrared surveillance; Laser modes; Laser transitions; Monitoring; Surface emitting lasers; Temperature measurement; Temperature sensors;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 1991. ICIASF '91 Record., International Congress on
Conference_Location
Rockville, MD
Type
conf
DOI
10.1109/ICIASF.1991.186235
Filename
186235
Link To Document