TY - GEN
T1 - Rarefaction effects in NASA arc jet testing at SCIROCCO facility
AU - Cinquegrana, Davide
AU - Votta, Raffaele
AU - Trifoni, Eduardo
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - In the frame of numerical rebuilding of SCIROCCO Plasma Wind Tunnel measurements, made during a facility characterization test campaign performed for NASA at increasing enthalpy and constant pressure, an important gap among measured and numerically predicted values of heat flux led to deep analyses of the models usually employed for test rebuilding. The Navier-Stokes model with chemical reacting non-equilibrium reactions, denoted a lack of physical accuracy due to local rarefaction effects, as certified by means of the continuum breakdown parameter. Then, a set of direct simulation Monte Carlo was performed to reduce the gap with the measured heat fluxes, and understand the real test chamber environment that was surrounding the probe. Finally, the numerical and experimental results, was related in terms of Knudsen number and coefficient of heat flux, to numerical and experimental results available in literature.
AB - In the frame of numerical rebuilding of SCIROCCO Plasma Wind Tunnel measurements, made during a facility characterization test campaign performed for NASA at increasing enthalpy and constant pressure, an important gap among measured and numerically predicted values of heat flux led to deep analyses of the models usually employed for test rebuilding. The Navier-Stokes model with chemical reacting non-equilibrium reactions, denoted a lack of physical accuracy due to local rarefaction effects, as certified by means of the continuum breakdown parameter. Then, a set of direct simulation Monte Carlo was performed to reduce the gap with the measured heat fluxes, and understand the real test chamber environment that was surrounding the probe. Finally, the numerical and experimental results, was related in terms of Knudsen number and coefficient of heat flux, to numerical and experimental results available in literature.
UR - http://www.scopus.com/inward/record.url?scp=85088070689&partnerID=8YFLogxK
U2 - 10.2514/6.2017-4450
DO - 10.2514/6.2017-4450
M3 - Conference contribution
AN - SCOPUS:85088070689
SN - 9781624104992
T3 - 47th AIAA Thermophysics Conference, 2017
BT - 47th AIAA Thermophysics Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 47th AIAA Thermophysics Conference, 2017
Y2 - 5 June 2017 through 9 June 2017
ER -