TY - GEN
T1 - A new concept of heat-flux probe for the Scirocco plasma wind tunnel
AU - Esposito, A.
AU - De Rosa, F.
AU - Filippis, F.
AU - Martucci, A.
AU - Graps, E.
AU - Trifoni, E.
PY - 2009
Y1 - 2009
N2 - Within the project "Calibration Heat Flux Probe", planned and developed within the program "Cibapark" by CIRA, a probe for stagnation point heat flux measurements, based on a "slug sensor" has been designed and realized. Such a sensor, particularly useful for high heat flux measurements arising in atmospherical re-entry conditions, offers great advantages compared with traditional alternatives (Gardon gage) such as low cost and prolonged durability. The sensor is made up of a metallic cylinder (slug) positioned in the probe's surface but physically separated by a thermal insulating material; the sensor's back face is equipped with a thermocouple. During the exposure to the heat flux, after a short transition period, temperature starts to grow linearly with time; by the slope of the curve and the knowledge of the thermo-phisical properties of the material (density and specific heat) the heat flux can be determined. The paper deals with the design, realization and test of this sensor for a test in the Scirocco plasma wind tunnel. Moreover, the heat flux evaluated by means of the thermocouple measurement has been also evaluated by means of a thermographic temperature measurement, and this method gave the same results.
AB - Within the project "Calibration Heat Flux Probe", planned and developed within the program "Cibapark" by CIRA, a probe for stagnation point heat flux measurements, based on a "slug sensor" has been designed and realized. Such a sensor, particularly useful for high heat flux measurements arising in atmospherical re-entry conditions, offers great advantages compared with traditional alternatives (Gardon gage) such as low cost and prolonged durability. The sensor is made up of a metallic cylinder (slug) positioned in the probe's surface but physically separated by a thermal insulating material; the sensor's back face is equipped with a thermocouple. During the exposure to the heat flux, after a short transition period, temperature starts to grow linearly with time; by the slope of the curve and the knowledge of the thermo-phisical properties of the material (density and specific heat) the heat flux can be determined. The paper deals with the design, realization and test of this sensor for a test in the Scirocco plasma wind tunnel. Moreover, the heat flux evaluated by means of the thermocouple measurement has been also evaluated by means of a thermographic temperature measurement, and this method gave the same results.
UR - http://www.scopus.com/inward/record.url?scp=77958563373&partnerID=8YFLogxK
M3 - Conference contribution
SN - 9781600867408
T3 - 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference
BT - 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference
T2 - 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference
Y2 - 19 October 2009 through 22 October 2009
ER -